RAE Table of Earth Satellites (extended)
(Compiled 2006)
Page 2006-1
Launchdate
Lifetime + Descent date
[Norad]
Shape and
weight (kg)
Descent date
Semi
major axis
(km)
Orbital
Argument
eccentricity of perigee
(deg)
2006 Jan 19.79
thick triangle 2.11x2.74
+ antenna
0.69 high
478 full
2.1 wide
401 empty
Solar escape orbit.#
2006 Mar
0.87
Year of Launch 2006
Name
[Launcher]
Fragments
Cospar ID
[Norad #] Launchsite
Cospar ID
New Horizons 1
[Atlas-V 551]
(AV-010)
D
2006-01 A
[28928]
CC-LC41
Size
(m)
Lifetime
Date of
orbital
determination
Orbital
Inclination
(deg)
Nodal
period
(min)
Perigee
height
(km)
Apogee
height
(km)
0.98
1.03
Kuiper Belt objects flyby from 2017 to 2020, then leaving the solar system.
Atlas-V 2nd stage
(Centaur)
2006-01 B
[28929]
2006 Jan 19.79
Cylinder
2000
11.74 long
3.05 dia
Heliocentric orbit
2007 Feb
at 2.8 AU in the asteroid belt
Atlas-V 3rd stage
(Star 48B)
2006-01 C
[28930]
2006 Jan 19.79
Cylinder
2137 full
126 empty
2.03 long
1.25 dia
Heliocentric orbit, after Jupiter flyby hyperbolic leaving the solar system
2007 Feb 28.07
Passed Jupiter at 2.8 million km
De-spin weights
2006-01 D, E 2006 Jan 19.79
[NNA]
Released from 2006-01 A after separation from 3rd stage
Heliocentric orbit, after Jupiter flyby hyperbolic leaving the solar system
ALOS (Daichi) *
2006-02 A
(Advanced Land Ob- [28931]
serving Satellite) TAN
[H-2A 2022 #8]
2006 Jan 24.06
Box+ 2 panels
± 4000
Palsar
Solar array
6.5x3.5
x4.5
8.9x3.1
22x3
2006
2006
2006
2006
2006
2006
24.11
26.72
7.31
13.45
13.49
13.51
98.23
98.22
98.22
98.22
98.19
98.22
98.68
98.73
98.75
99.08
98.78
98.67
7075
7076
7077
7094
7079
7074
695
697
697
690
700
689
697
699
701
740
700
701
0.0001
0.0001
0.0002
0.004
0
0.0009
138
154
142
103
341
162
H-2A 2nd stage
2006-02 B
[28932]
2006 Jan 24.06
Cylinder
11.0 long
4.0 dia
2006 Jan 24.11
2006 Jan 24.65
98.22
98.21
97.08 6997
97.17 7001
546
547
692
699
0.010
0.011
127
123
Fragments
2006-02 C-AA 23 pieces, 21 have decayed
For orbital information see extra pages at end of year
Echostar 10
[Zenit-3 SL]
2006-03 A
[28935]
ODS
2006 Feb 15.98
> million years
Box+ 2 panels
+ 4 dishes
4333
2006
2006
2006
2006
2006
2006
2006
2006
2006
Zenit-3 SL
3rd Stage
(Block DM-SL)
2006-03 B
[28936]
2006 Feb 15.98
Cylinder
2140
6.22 long
3.7 maxdia
Jan
Jan
Feb
Feb
Feb
Feb
Feb
Feb
Feb
Feb
Feb
Feb
Feb
Feb
Mar
15.99
16.38
17.29
17.78
20.00
21.97
22.96
27.57
1.31
0
0.06
0.02
0.09
0.04
0.04
0.03
0.04
0.04
2006 Feb 17.29
0.06
658.55
766.55
792.50
945.77
1196.97
1433.12
1435.97
1436.12
25074
26278
28368
31917
37344
42107
42162
42165
656.03 25010
#
Gravity assist by Jupiter 2007 Feb 28.24 at 2.305 million km; flyby of Pluto 2015 July 14.
*
Space Track has changed the TLE’s for A and B on 2006 Jan 26. The first few days A had the TLE’s for B and vice-versa.
2014 - Version 1-13
180
1707
4124
8309
15408
26258
35688
35780
35783
2105
35684
35675
35670
35668
35672
35768
35788
35790
0.678
0.600
0.482
0.317
0.126
0.001
0.0001
0.00009
203
184
168
25
350
337
302
216
1654
35609
0.679
153
RAE Table of Earth Satellites (extended)
(Compiled 2006)
Page 2006-2
Launchdate
Lifetime + Descent date
[Norad]
Shape and
weight (kg)
Descent date
Size
(m)
Lifetime
Date of
orbital
determination
Orbital
Inclination
(deg)
Semi
major axis
(km)
Year of Launch 2006
Name
[Launcher]
Fragments
D
D
Cospar ID
[Norad #] Launchsite
Cospar ID
241
35751
35773
35771
35775
34914
35773
35813
35807
35797
0.724
0.0003
0.0005
0.0004
0.0003
179
79
221
261
329
243
244
35790
35750
0.729
0.728
179
179
Box+2 antennea
+solar array+
boom+solarsail
4650 full
4x4x6
2.4x7.8
15.1+3 dia
30 span
2006
2006
2006
2006
2006
18.51
24.17
27.50
1.13
3.14
28.52
0.03
0.02
0.02
0.04
H-2A 2nd stage
2006-04 B
[28938]
2006 Feb 18.27
> million years
Cyl + cone
3000?
10.6 long
4 maxdia
2006 Feb 18.51
2006 Feb 18.80
28.50
28.53
Astro F
(Akari)
[M-V #8]
2006-05 A
[28939]
KAG
2006 Feb 21.89
8-sided drum
+ cylinder
+ panel
952
2.026x1.880 2006 Feb 22.00
3.675 high 2006 Feb 27.80
5.5 span
2006 Feb 28.93
2006 Mar 2.28
2006 Mar 2.49
2006 Mar 3.65
2006 Mar 3.86
2006 Mar 4.75
2006 Apr 2.05
98.20
98.20
98.20
98.20
98.20
98.17
98.20
98.20
98.20
94.82
95.65
96.55
97.47
98.38
99.02
99.02
98.78
98.90
6888
6929
6972
7016
7060
7091
7090
7079
7084
299
384
470
558
647
700
707
694
698
721
716
716
716
716
724
716
708
713
0.031
0.024
0.018
0.011
0.005
0.002
0.0006
0.001
0.001
147
123
119
114
113
214
118
263
172
Solarsail
2006-05 B
[28940]
2006 Feb 21.89
104 days
2006 Jun 5
Mylar foil
10 dia
2006 Feb 22.13
2006 Jun 5.01
98.20
98.15
94.73 6884
88.50 6579
302
187
709
214
0.030
0.002
147
165
Cute-1.7
2006-05 C
[28941]
2006 Feb 21.89
Cube
3.63
0.10x0.10
x0.20
2006 Feb 22.07
98.19
94.70 6883
301
707
0.030
146
M-V 3rd stage
2006-05 D
[28942]
2006 Feb 21.89
Sphere + cone
11000 full
1000 empty
3.60 long
2.20 dia
2006 Feb 22.26
2006 Feb 22.33
98.19
98.18
94.73 6884
94.73 6884
303
300
709
712
0.030
0.030
146
145
Lens cover
2006-05 E
[29054]
2006 Feb 21.89
2006 Apr 17.59
98.20
98.93 7086
699
715
0.001
130
Arabsat-4A *
[Proton-M
Breeze-M]
2006-06 A
2006 Feb 28.84
[28943]
24 days
BAI-LC200/39 2006 Mar 24
2006 Mar 1.08
2006 Mar 23.54
51.52
51.56
274.13 13979
273.83 13969
505
492
14695
14688
0.508
0.508
5
17
2006 Mar 1.27
51.53
274.13 13979
505
14695
0.508
5
Fragments
*
Orbital
Argument
eccentricity of perigee
(deg)
2006 Feb 18.27
> million years
2006 Feb 28.84
disintegrated
Cylinder
1220
2006-06 C-DG 101 pieces, 5 have decayed
2.62 long
2.4 dia
23956
42141
42172
42168
42165
Apogee
height
(km)
2006-04 A
[28937]
TAN
Proton-M 4th stage 2006-06 B
(Breeze-M) *
[28944]
615.00
1434.85
1436.45
1436.23
1436.08
Perigee
height
(km)
MTSAT-2
(Himawari 7)
[H-2A 2024 #9]
Box+ 2 panels
+ 2 antennae
3341
Feb
Feb
Feb
Mar
Mar
Nodal
period
(min)
632.00 24395
631.22 24375
For orbital information see extra pages at end of year
4th burn of the Breeze-M didn’t occur (properly). Satellite left in a low orbit; de-orbited by satellite owner.
On 2007 Mar 19.716 the 4th stage fragmented, the event was observed and filmed from Australia. More than 1100 fragments were observed by radar.
2014 - Version 1-13
RAE Table of Earth Satellites (extended)
(Compiled 2006)
Page 2006-3
Launchdate
Lifetime + Descent date
[Norad]
Shape and
weight (kg)
Descent date
Semi
major axis
(km)
Year of Launch 2006
Name
[Launcher]
Fragments
Cospar ID
[Norad #] Launchsite
Cospar ID
Size
(m)
Lifetime
Date of
orbital
determination
Orbital
Inclination
(deg)
Perigee
height
(km)
Apogee
height
(km)
Orbital
Argument
eccentricity of perigee
(deg)
Spainsat
[Ariane-5 ECA]
(527 – V170)
2006-07 A
[28945]
KOU-ELA3
2006 Mar 11.94
> million years
Box + 2 panels 5.4x2.8
3683 full
x2.2
1467 empty
31.4 span
2006
2006
2006
2006
2006
2006
12.18
14.40
15.80
16.56
17.71
29.29
5.04
0.68
0.13
0.02
0.04
0.06
630.92
1071.27
1388.93
1393.08
1434.30
1436.08
24367
34681
41237
41319
42130
42165
268
20852
33954
34118
35738
35776
35709
35753
35762
35762
35764
35796
0.727
0.215
0.022
0.020
0.0003
0.0002
178
181
192
207
282
327
Hot Bird 7A
2006-07 B
[28946]
2006 Mar 11.94
> million years
Box + 2 panels 3.7x1.8
4100 full
x2.3
1740 empty
36.9 span
2006 Mar 12.18
2006 Mar 20.02
2006 Mar 31.90
5.04
0.10
0.06
631.43 24381
1426.25 41972
1436.08 42165
269
35593
35751
35735
35594
35821
0.727
0.00001
0.0008
178
0
7
Sylda upper part
2006-07 C
[28947]
2006 Mar 11.94
Barrel shaped
500?
2006 Mar 12.18
5.03
632.63 24412
276
35790
0.727
178
Ariane-5 2nd stage 2006-07 D
[28948]
2006 Mar 11.94
Drum-cone
2880
3.5 long
3.94 dia
2006 Mar 12.17
5.17
623.78 24183
267
35343
0.725
180
Space Technology 5 2006-08 A
ST-5 A (P-495)
[28980]
[L1011/Pegasus XL] VDB
2006 Mar 22.59
8-sided cyl +
magn. boom
25
0.43 dia
0.48 high
2006 Mar 22.65
2006 Mar 23.22
105.62
105.63
137.02 8804
137.03 8805
298
302
4554
4550
0.242
0.241
157
157
Space Technology 5 2006-08 B
ST-5 B (P-495)
[28981]
2006 Mar 22.59
8-sided cyl +
magn. boom
25
0.43 dia
0.48 high
2006 Mar 22.84
2006 Mar 23.21
105.63
105.61
136.53 8784
137.00 8804
297
303
4514
4547
0.240
0.241
158
157
Space Technology 5 2006-08 C
ST-5 C (P-495)
[28982]
2006 Mar 22.59
8-sided cyl +
magn. boom
25
0.43 dia
0.48 high
2006 Mar 22.84
2006 Mar 23.22
105.62
105.62
136.95 8802
137.05 8806
299
303
4547
4551
0.241
0.241
157
157
Pegasus-XL
3rd stage
2006-08 D
[28983]
2006 Mar 22.59
Cylinder
176
2.08 long
0.97 dia
2006 Mar 23.22
105.63
137.20 8812
303
4564
0.242
156
Fragment
2006-08 E
[29535]
2006 Sep 6.95
105.66
129.63 8485
301
3912
0.213
312
2006-09 A
[28996]
BAI-LC1
2006 Mar 30.10
182.95 days
2006 Sep 29.05
Cyl+ 2 panels+ 7.5 long
2006 Mar 30.19
beehive+sphere 2.3 to
2006 Mar 30.74
7250
2.72 maxdia 2006 Mar 31.36
2006 Apr 1.16
2006 Apr 2.45
2006 Sep 28.47
2006 Sep 29.02
51.64
51.65
51.64
51.64
51.64
51.64
51.65
88.87
90.23
90.27
91.43
91.43
91.35
91.35
6597
6664
6666
6723
6723
6719
6719
195
259
267
339
338
332
334
241
312
308
351
351
349
347
0.004
0.004
0.003
0.0009
0.0009
0.001
0.001
84
165
169
67
71
36
22
D
Soyuz-FG 3rd stage 2006-09 B
(Block I)
[28997]
2006 Mar 30.10
3 days
2006 Apr 2
Cylinder
2400?
51.64
51.62
88.80 6593
87.43 6526
195
145
235
150
0.003
0.0004
76
67
*
Expedition 13 crew of two cosmonauts (Vinogradov and Williams) and Brazilian Portes docked with ISS (Pirs port) 2006 Apr 01.18;
Portes returned to Earth 2006 Apr 8 with Expedition 12 crew in Soyuz-TMA 7. Soyuz-TMA 8 undocked 2006 Sep 28.91 and landed with Vinogradov, Williams
And space-participant Anoush Ansari, who flew to ISS with Soyuz-TMA 9.
D Soyuz-TMA 8 *
3M [Soyuz-FG]
R
2014 - Version 1-13
8.1 long
2.66 dia
Mar
Mar
Mar
Mar
Mar
Mar
Nodal
period
(min)
2006 Mar 30.19
2006 Apr 2.35
RAE Table of Earth Satellites (extended)
(Compiled 2006)
Page 2006-4
Launchdate
Lifetime + Descent date
[Norad]
Shape and
weight (kg)
Descent date
Semi
major axis
(km)
2006-10 A
[29045]
ODS
2006 Apr 12.98
> million years
Box+ 2 panels
4401
Zenit-3 SL
3rd stage
(Block-DM SL)
2006-10 B
[29046]
2006 Apr 12.98
Cylinder
2140
Formosat 3A *
2006-11 A
[29047]
VDB-SLC8
2006 Apr 15.07
Formosat 3B *
2006-11 B
[29048]
Formosat 3C *
Year of Launch 2006
Name
[Launcher]
Fragments
Date of
orbital
determination
Orbital
Inclination
(deg)
Perigee
height
(km)
Apogee
height
(km)
Orbital
Argument
eccentricity of perigee
(deg)
2006
2006
2006
2006
2006
2006
2006
2006
2006
13.16
14.53
16.48
18.61
20.13
24.73
26.29
27.58
2.65
0.01
0.09
0.05
0.01
0.02
0.02
0.03
0.01
0.04
1701
3482
11665
21233
35673
35737
35760
35782
35782
35665
35660
35652
35656
35756
35768
35789
35789
35791
0.678
0.620
0.399
0.207
0.001
0.0004
0.0003
0.00007
0.0001
75
178
171
288
152
288
263
108
221
2006 Apr 13.16
0.04
656.23 25015
1665
35608
0.678
181
Disc + 2
round panels
69.33
2006 Apr 15.24
72.02
94.95 6895
496
536
0.003
180
2006 Apr 15.07
Disc + 2
round panels
69.33
2006 Apr 15.44
2006 Apr 15.97
72.03
72.02
95.02 6898
94.98 6896
505
495
534
540
0.002
0.003
193
180
2006-11 C
[29049]
2006 Apr 15.07
Disc + 2
round panels
69.33
2006 Apr 15.44
2006 Apr 15.84
72.03
72.02
95.13 6904
94.98 6896
508
495
542
540
0.002
0.003
168
180
Formosat 3D *
2006-11 D
[29050]
2006 Apr 15.07
Disc + 2
round panels
69.33
2006 Apr 15.44
2006 Apr 16.10
72.02
72.02
95.13 6903
94.98 6896
507
495
543
540
0.003
0.003
168
180
Formosat 3E *
2006-11 E
[29051]
2006 Apr 15.07
Disc + 2
round panels
69.33
2006 Apr 15.44
2006 Apr 16.04
72.03
72.02
95.03 6898
94.98 6896
504
496
535
539
0.002
0.003
184
178
Formosat 3F *
2006-11 F
[29052]
2006 Apr 15.07
Disc + 2
round panels
69.33
2006 Apr 15.44
2006 Apr 16.10
72.06
72.02
94.95 6895
94.98 6896
508
495
524
540
0.001
0.003
254
179
Minotaur
4th stage
(Orion 38)
2006-11 G
[29053]
2006 Apr 15.07
Cylinder
2006 Apr 15.44
2006 Apr 15.97
2006 Apr 16.04
72.08
72.03
72.02
95.02 6898
94.97 6896
94.98 6896
482
491
495
557
543
540
0.005
0.004
0.003
335
180
180
JCSat 9
[Zenit-3 SL]
*
Cospar ID
[Norad #] Launchsite
Cospar ID
Size
(m)
Lifetime
26.4 span
6.22 long
3.7 maxdia
1.76 long
1.27 dia
Apr
Apr
Apr
Apr
Apr
Apr
Apr
Apr
May
Nodal
period
(min)
658.07
693.35
863.47
1077.85
1432.42
1434.40
1435.50
1436.07
1436.10
25062
25950
30037
34823
42093
42132
42153
42164
42165
Six micro-satellites in Constellation Observing System for Meteorology, Ionosphere & Climate; joined Taiwan-USA program.
All six satellites were deployed within 5 minutes from 14m25s to 19m19s after lift-off.
2014 - Version 1-13
RAE Table of Earth Satellites (extended)
(Compiled 2006)
Page 2006-5
Launchdate
Lifetime + Descent date
[Norad]
Shape and
weight (kg)
Descent date
Size
(m)
Lifetime
Date of
orbital
determination
Orbital
Inclination
(deg)
Semi
major axis
(km)
Year of Launch 2006
Name
[Launcher]
Fragments
Cospar ID
[Norad #] Launchsite
Cospar ID
Orbital
Argument
eccentricity of perigee
(deg)
6470
8704
12747
20286
30444
35695
35714
35780
35782
36240
35777
35777
35773
35771
35767
35779
35790
35791
0.537
0.473
0.376
0.225
0.067
0.0009
0.0008
0.0001
0.0001
181
181
181
182
188
254
290
147
102
6069
35029
0.538
180
2006 Apr 20.85
Box+ 2 panels
4332
3.4x2.8
4.5-7.4 hg
26.2 span
2006
2006
2006
2006
2006
2006
2006
2006
2006
21.13
23.73
24.85
26.08
27.52
30.35
3.45
4.26
5.75
23.82
17.97
12.04
5.88
1.50
0.23
0.21
0.23
0.21
Atlas-5 2nd stage
(Centaur)
2006-12 B
[29056]
2006 Apr 20.85
Cylinder
2100?
12.68 long
3.05 dia
2006 Apr 21.63
24.67
D
Progress-M 56 *
[Soyuz-U]
2006-13 A
[29057]
BAI-LC1
2006 Apr 24.67
147.35 days
2006 Sep 19.02
Cyl+ 2 panels+ 7.9 long
2006 Apr 24.72
beehive+sphere 2.12 maxdia 2006 Apr 24.86
7265
2006 Apr 24.92
2006 Apr 26.66
2006 Sep 18.78
51.62
51.61
51.63
51.64
51.64
88.55
89.53
90.28
91.38
91.37
6581
6630
6667
6721
6720
189
218
248
336
334
216
285
329
348
349
0.002
0.005
0.006
0.0009
0.001
67
184
124
152
359
D
Soyuz-U 3rd stage
(Block I)
2006-13 B
[29058]
2006 Apr 24.67
2 days
2006 Apr 26
Cylinder
2400?
2006 Apr 24.85
2006 Apr 26.92
51.62
51.61
88.50 6579
87.12 6510
188
119
213
144
0.002
0.002
69
167
Eros B1 $
[Topol]
2006-14 A
[29079]
SVO
2006 Apr 25.70
2006 Apr 25.76
97.32
94.78 6886
503
513
0.0007
106
Topol 3rd stage
2006-14 B
[29080]
2006 Apr 25.70
2006 Apr 25.76
97.32
94.82 6888
503
516
0.001
94
Remote Sensing
Satellite 1
(Yaogan 1)
[CZ-4B]
2006-15 A
[29092]
WUZ
2006 Apr 26.95
2006 Apr 27.00
2006 Apr 27.13
97.81
97.80
96.92 6990
96.98 6993
601
603
621
626
0.001
0.002
351
4
CZ-4B 3rd stage
2006-15 B
[29093]
2006 Apr 26.95
2006 Apr 26.99
97.85
95.40 6916
452
624
0.012
34
Fragment
2006-15 C-J
5 pieces, 1 has decayed
732.90 26927
280
Cylinder
1.58 dia
2720
Cylinder
1727
4.93 long
2.9 dia
Replacement for Astra-1K, which was lost in a Proton launch failure 2002 Oct.
Docked with ISS (Zvezda aft port) 2006 Apr 26.74; undocked 2006 Sep 19.02
Israeli photo-reconnaissance satellite launched by Russia.
2014 - Version 1-13
27734
28619
30641
34408
39486
42110
42125
42164
42165
Apogee
height
(km)
2006-12 A
[29055]
CC-LC41
#
*
$
766.07
803.05
889.63
1058.65
1301.45
1433.28
1434.07
1436.03
1436.10
Perigee
height
(km)
Astra-1KR #
[Atlas 5-411]
(AV-008)
8.1 long
2.66 dia
Apr
Apr
Apr
Apr
Apr
Apr
May
May
May
Nodal
period
(min)
For orbital information see extra pages at end of year
RAE Table of Earth Satellites (extended)
(Compiled 2006)
Page 2006-6
Launchdate
Lifetime + Descent date
[Norad]
Shape and
weight (kg)
Descent date
Semi
major axis
(km)
Box+ 2 panels
Year of Launch 2006
Name
[Launcher]
Fragments
Cospar ID
[Norad #] Launchsite
Cospar ID
Size
(m)
Lifetime
Date of
orbital
determination
Orbital
Inclination
(deg)
Nodal
period
(min)
Perigee
height
(km)
Apogee
height
(km)
Orbital
Argument
eccentricity of perigee
(deg)
2006
2006
2006
2006
2006
2006
Apr
Apr
May
May
May
May
28.43
28.67
12.63
26.26
27.63
28.32
98.09
98.23
98.23
98.23
98.25
98.24
93.15
98.52
98.53
98.70
98.82
98.82
6807
7067
7067
7075
7081
7081
173
687
685
695
700
701
684
689
692
699
704
703
0.038
0.0002
0.0005
0.0003
0.0002
0.0002
178
229
199
114
94
73
2006
2006
2006
2006
2006
Apr
Apr
May
May
Jun
28.60
29.49
31.48
31.68
1.37
98.24
98.24
98.24
98.23
98.24
98.53
98.55
98.78
98.82
98.82
7067
7068
7079
7081
7081
688
689
969
700
701
689
689
706
704
703
0.00008
0.00004
0.0007
0.0002
0.0002
198
346
159
63
89
2006 Apr 28.72
2006 Jun 1.56
2006 Jul 6.50
102.78
102.77
102.76
93.00 6800
91.23 6714
87.37 6523
206
197
103
637
473
185
0.032
0.021
0.006
114
11
250
2006 Apr 28.60
98.25
98.48 7064
684
688
0.0003
285
2012 Jun 27.02
2012 Sep 8.63
98.41
98.35
95.48 6920
88.58 6583
534
189
549
220
0.001
0.002
124
6
2006
2006
2006
2006
2006
2006
2006
2006
2006
2006
2006
2006
2006
2006
2006
67.17
67.15
67.15
67.15
67.15
67.15
67.15
67.15
67.14
67.15
67.14
67.14
67.14
67.14
67.14
89.57
89.40
89.92
89.23
89.92
89.92
89.47
89.60
89.32
89.93
89.28
89.82
89.40
89.15
88.88
6632
6623
6649
6615
6649
6649
6627
6633
6619
6649
6618
6644
6623
6611
6598
168
166
186
178
189
191
184
187
184
176
173
181
179
172
168
338
323
355
296
352
350
312
322
297
366
306
350
311
292
270
0.013
0.012
0.013
0.009
0.012
0.012
0.010
0.010
0.009
0.014
0.010
0.013
0.010
0.009
0.008
91
89
70
51
73
73
57
61
53
129
110
125
112
119
116
CloudSat
[Delta-2
(7420-10C)]
2006-16 A
[29107]
VDB-SLW2W
2006 Apr 28.42
Calypso
2006-16 B
[29108]
2006 Apr 28.42
Delta-2 2nd stage
(Centaur) *
2006-16 C
[29109]
2006 Apr 28.42
69 days
2006 Jul 6
Delta-2 DPAF *
2006-16 D
[29110]
2006 Apr 28.42
D
Fragment
2006-16 E
[38545]
D
Cosmos 2420
(Kobalt)
[Soyuz-U]
2006-17 A
[29111]
PLE-LC16
2006 May 3.73
77 days
2006 Jul 19
D
Soyuz-U 3rd stage
(Block I)
2006-17 B
[29112]
2006 May 3.73
5 days
2006 May 8
Cylinder
2400?
8.1 long
2.66 dia
2006 May 3.91
2006 May 6.20
2006 May 7.43
67.15
67.15
67.15
89.25 6624
88.72 6590
87.92 6550
168
156
140
323
266
203
0.012
0.008
0.005
90
89
88
D
D
Fragment
2006-17 C
2006-17 D
[29113]
[29258]
2006 May 6
2006 Jul 20
3 days
78 days
2006-17 E
[29259]
2006
2006
2006
2006
67.15
67.14
67.03
67.16
88.47
88.57
87.92
87.35
145
164
128
115
252
244
214
172
0.008
0.006
0.007
0.004
93
118
347
124
D
*
Cylinder
919
2012 Sep 8
5.88 long
2.44 dia
2325 days
May
May
May
May
May
May
Jun
Jun
Jun
Jun
Jul
Jul
Jul
Jul
Jul
May
Jul
Jul
Jul
3.85
6.42
6.72
24.91
25.16
25.40
8.86
8.99
17.00
17.43
2.05
2.31
14.46
14.72
19.71
5.34
19.83
20.13
20.13
6577
6582
6550
6522
Space-Track interchanged on 2006 May 2 the orbital elements for the Delta-2 2nd stage and the DPAF (Double Payload Adapter Facility).
2014 - Version 1-13
RAE Table of Earth Satellites (extended)
(Compiled 2006)
Page 2006-7
Launchdate
Lifetime + Descent date
[Norad]
Shape and
weight (kg)
Descent date
Size
(m)
Lifetime
Date of
orbital
determination
Orbital
Inclination
(deg)
Semi
major axis
(km)
Year of Launch 2006
Name
[Launcher]
Fragments
Cospar ID
[Norad #] Launchsite
Cospar ID
27300
30851
38143
40748
42162
42164
Apogee
height
(km)
Orbital
Argument
eccentricity of perigee
(deg)
6670
13788
28367
33570
35768
35779
35172
35157
35162
35168
35798
35791
0.522
0.346
0.089
0.020
0.0004
0.0001
179
180
190
225
136
144
2006-18 A
[29155]
CC-LC37B
2006 May 24.92
> million years
Box + panel
3133 full
1800 bol
4.2 long
1.88 wide
8.23 span
2006
2006
2006
2006
2006
2006
25.14
27.98
30.06
1.70
4.61
18.46
12.08
6.21
1.10
0.30
0.54
0.51
Delta-4 2nd stage
2006-18 B
[29156]
2006 May 24.92
Cylinder
12 long
2.44 dia
2006 May 27.25
13.08
745.82 27243
6588
35139
0.524
180
Kompass 2 *
[Shtil 1]
2006-19 A
[29157]
2006 May 26.78
0.5x1.0x1.0 2006 May 26.96
79.04
93.80 6839
406
515
0.008
111
Shtil 1 3rd stage?
2006-19 C
[29159]
2006 May 26.78
3094 days
2014 Nov 14
2006 May 27.03
2014 Nov 14.42
78.91
78.84
93.52 6826
87.07 6508
399
124
494
134
0.007
0.0008
117
345
Fragments
D
2006-19 B
2006-19 D
[29158]
[29160]
2006 Oct 15
142 days
D
2006-19 E
[29161]
2006
2006
2006
2006
2007
93.45
93.50
89.08
93.53
88.75
6822
6825
6608
6826
6591
402
401
218
401
204
484
491
240
493
221
0.006
0.007
0.002
0.007
0.001
113
109
157
107
196
Satmex 6
[Ariane-5 ECA]
(V171 / 5-027)
2006-20 A
[29162]
KOU-ELA3
Thaicom 5
Sylda upper part
*
748.15
898.78
1235.63
1364.30
1435.93
1436.03
Perigee
height
(km)
GOES-13
[Delta-4 M+(4.2)]
(Delta 4240)
D
May
May
May
Jun
Jun
Jun
Nodal
period
(min)
82
2007 Mar 21
299 days
May
May
Oct
May
Mar
26.84
27.55
15.48
28.79
19.98
78.85
78.87
78.84
78.90
78.88
2006 May 27.88
> million years
Box+ 2 panels
5456 full
2310 empty
7.4x2.8x3.4 2006 May
31.4 span
2006 May
2006 May
2006 Jun
2006 Jun
2006 Jun
2006 Jun
28.12
29.55
30.01
1.60
1.90
3.79
7.59
7.52
3.08
0.47
0.05
0.04
0.05
0.05
628.78
789.15
1208.87
1391.68
1399.55
1432.32
1436.10
24313
28288
37891
41291
41447
42091
42165
236
8046
26697
34099
34413
35704
35781
35632
35772
35728
35725
35723
35720
35791
0.728
0.490
0.120
0.020
0.016
0.0002
0.0001
180
178
183
213
261
270
280
2006-20 B
[29163]
2006 May 27.88
> million years
Box+ 2 panels
2766 full
1220 empty
3.7x3.3x2.2 2006 May 28.56
26.2 span
2006 Jun 3.80
2006 Jun 5.00
6.97
0.15
0.14
631.85 24391
1436.98 42182
1432.28 42090
252
35355
35387
35774
36252
36036
0.728
0.011
0.008
178
268
279
2006-20 C
[29164]
2006 May 27.88
Barrel shaped
500?
2006 May 28.56
2007 Feb 3.79
6.99
6.74
631.42 24380
551.03 22264
250
190
35753
31579
0.728
0.705
178
27
Ariane-5 2nd stage 2006-20 D
+ VEB
[29165]
2006 May 27.88
Drum-cone
2880
Cylinder
950
2006 May 28.56
2007 Feb 1.70
6.98
7.24
632.50 24408
619.05 24061
254
202
35806
35163
0.728
0.727
178
22
3.5 long
3.94 dia
1.13 high
3.94 dia
Complex Orbital Magneto-Plasma Autonomous Small Satellite (Compass 2) was launched from the Russian submarine Ekaterinburg in the Barents Sea.
2014 - Version 1-13
Year of Launch 2006
Name
[Launcher]
Fragments
D
Cospar ID
[Norad #] Launchsite
Cospar ID
Launchdate
Lifetime + Descent date
[Norad]
Resurs-DK 1
[Soyuz-U]
2006-21 A
[29228]
BAI
2006 Jun 15.17
Soyuz-U 3rd stage
(Block I)
2006-21 B
[29229]
2006 Jun 15.17
13 days
2006 Jun 28
KazSat 1
[Proton-K]
2006-22 A
[29230]
BAI
2006 Jun 17.95
> million years
RAE Table of Earth Satellites (extended)
(Compiled 2006)
Page 2006-8
Shape and
weight (kg)
Descent date
Semi
major axis
(km)
Size
(m)
Lifetime
6800
Cylinder
2400?
8.1 long
2.66 dia
Date of
orbital
determination
Orbital
Inclination
(deg)
2006
2006
2006
2006
15.45
16.59
18.60
18.66
69.95
69.94
69.81
69.94
89.83
89.85
93.45
94.00
2006 Jun 15.52
2006 Jun 28.57
69.97
69.95
2006
2006
2006
2006
2006
2006
18.00
19.60
27.82
8.37
19.82
24.30
51.50
0.01
0.01
0.03
0.01
0.01
Jun
Jun
Jun
Jun
Jun
Jun
Jun
Jul
Jul
Jul
Nodal
period
(min)
Perigee
height
(km)
Apogee
height
(km)
Orbital
Argument
eccentricity of perigee
(deg)
6644
6646
6822
6849
195
191
412
355
336
343
474
585
0.010
0.011
0.005
0.017
60
59
104
128
89.90 6648
87.33 6521
192
133
347
152
0.012
0.001
58
21
213
35381
35766
35726
35746
35781
35782
35781
35824
35729
35789
35791
0.730
0.005
0.0007
0
0.0005
0.0001
1
117
281
64
110
318
631.25
1425.63
1436.53
1433.08
1435.13
1436.08
24376
41960
42173
42106
42126
42165
D
Proton-K 4th stage 2006-22 B
Casing
[29231]
2006 Jun 17.95
1 day
2006 Jun 18
Hollow cyl
800?
4.0 long
3.7 dia
2006 Jun 18.19
2006 Jun 18.61
51.56
51.56
88.38 6573
87.85 6547
180
154
209
182
0.002
0.002
263
277
D
Proton-K 3rd stage 2006-22 C
[8S812)
[29232]
2006 Jun 17.95
3 days
2006 Jun 20
Cylinder
4185
4 long
4.1 dia
2006 Jun 18.25
2006 Jun 20.26
51.57
51.56
88.22 6565
87.03 6506
154
114
218
142
0.005
0.002
274
267
Proton-K 4th stage 2006-22 D
(Block DM)
[29233]
2006 Jun 17.95
> million years
Cylinder
2350?
6.22 long
3.7 dia
2006 Jun 18.01
0.01
1436.45 42172
35764
35822
0.0007
215
Fragments
2006-22 E-H
4 pieces, all have decayed
For orbital information see extra pages at end of year
Galaxy 16
[Zenit-3SL]
2006-23 A
[29236]
ODS
2006 Jun 18.33
> million years
2006
2006
2006
2006
2006
2006
2006
2006
Zenit-3SL 3rd stage 2006-23 B
(Block-DM SL)
[29237]
2014 - Version 1-13
2006 Jun 18.33
4640
Cylinder
2140
6.22 long
3.7 dia
Jun
Jun
Jun
Jun
Jun
Jun
Jul
Aug
18.82
19.62
21.60
22.40
26.60
28.85
16.15
15.30
0.05
0.09
0.15
0.24
0.11
0.11
0.06
0.02
2006 Jun 18.82
0.11
668.98
753.92
1077.13
1375.82
1427.60
1436.07
1440.42
1436.08
25338
27440
34808
40976
41998
42164
42249
42165
666.38 25272
2272
6508
21227
33579
35547
35766
35802
35776
35647
35614
35631
35617
35692
35805
35940
35796
0.659
0.530
0.207
0.025
0.002
0.0005
0.002
0.0002
181
224
193
187
121
45
328
303
2198
35590
0.661
195
RAE Table of Earth Satellites (extended)
(Compiled 2006)
Page 2006-9
Launchdate
Lifetime + Descent date
[Norad]
Shape and
weight (kg)
Descent date
Semi
major axis
(km)
Orbital
Argument
eccentricity of perigee
(deg)
USA 187
2006-24 A
(MiTEx) *
[29240]
[Delta-2 7925-9.5] CC-LC17A
2006 Jun 21.93
Ring with
spheres
No TLE available; orbits from amateur satellite observations
2009 Feb 1.23
2.44
1428.25 42011 35624 35640 0.0002
2010 Jan 1.00
1.55
1434.03 42125 35725 35767 0.0005
USA 188
OSC Small Sat
2006-24 B
[29241]
2006 Jun 21.93
Box+ 2 panels
227
Geostationary orbit
USA 189
LMC Small Sat
2006-24 C
[29242]
2006 Jun 21.93
Box+ 2 panels
227
No TLE available; orbits from amateur satellite observations
2009 Apr 21.66
2.26
1384.48 41149 34751 34789 0.0005
Delta-2 2nd stage
(Centaur)
2006-24 D
[29243]
2006 Jun 21.93
Cylinder
919
5.88 long
2.44 dia
Delta-2 3rd stage
(PAM-D)
2006-24 E
[29244]
2006 Jun 21.93
Cone-cyl
205
2.29 long
1.50 dia
D
Progress-M 57 **
[Soyuz-U]
2006-25 A
[29245]
BAI-LC1
2006 Jun 24.63
207 days
2007 Jan 17
Cyl+ 2 panels+ 7.9 long
2006 Jun 24.62
beehive+sphere 2.12 maxdia 2006 Jun 25.39
7265
2007 Jan 17.00
51.29
51.63
51.63
88.10 6559
89.77 6641
91.32 6718
140
255
323
220
271
356
0.006
0.001
0.002
306
350
98
D
Soyuz-U 3rd stage
(Block I)
2006-25 B
[29246]
2006 Jun 24.63
3 days
2006 Jun 27
Cylinder
2400?
2006 Jun 24.87
2006 Jun 26.89
2006 Jun 27.32
51.63
51.62
51.62
88.50 6579
87.85 6547
87.47 6528
187
164
148
213
172
150
0.002
0.001
0.0001
62
63
47
Cosmos 2421
[Tsyklon-2]
2006-26 A
[29247]
BAI
2006 Jun 25.17
2006 Jun 25.29
65.05
92.77 6789
404
416
0.0009
285
Tsyklon-2
2nd stage
2006-26 B
[29248]
2006 Jun 25.17
< 1 day
2006 Jun 25
2006 Jun 25.59
65.07
87.93 6551
92
252
0.012
56
Fragments
2006-26 C-WE 329 pieces, 43 have decayed
Year of Launch 2006
Name
[Launcher]
Fragments
D
Cospar ID
[Norad #] Launchsite
Cospar ID
Cylinder
4000
Size
(m)
Lifetime
8.1 long
2.66 dia
10.9 long
3 dia
Date of
orbital
determination
Orbital
Inclination
(deg)
Nodal
period
(min)
Apogee
height
(km)
For orbital information see extra pages at end of year
* Micro-satellite Technology Experiment; NRL build upper stage to put the two microsats in geostationary orbit.
** Docked with ISS (PIRS port) 2006 Jun 26.68; undocked 2007 Jan 17
2014 - Version 1-13
Perigee
height
(km)
123
22
194
Year of Launch 2006
Name
[Launcher]
Fragments
Cospar ID
[Norad #] Launchsite
Cospar ID
Launchdate
Lifetime + Descent date
[Norad]
RAE Table of Earth Satellites (extended)
(Compiled 2006)
Page 2006-10
Shape and
weight (kg)
Descent date
Semi
major axis
(km)
Orbital
Argument
eccentricity of perigee
(deg)
Size
(m)
Lifetime
Date of
orbital
determination
Orbital
Inclination
(deg)
2006
2006
2009
2010
28.16
28.19
28.37
13.12
62.5
62.4
63.26
63.26
2009 May 19.75
62.43
Perigee
height
(km)
Apogee
height
(km)
717.85 26558
717.78 26556
193
1113
1397
1989
2215
37610
38961
38365
0.707
0.685
#
#
272 ##
273 ##
661.77 25156
1531
36023
0.686
280 ##
USA 184 (NRO L-22}$ 2006-27 A
[Delta-4 M+(4,2)] [29249]
VDB-SLC6
2006 Jun 28.15
Delta-4 2nd stage
2006-27 B
[29250]
2006 Jun 28.15
D STS-121 **
7M Discovery F32
R [Shuttle]
2006-28 A
[29251]
CC-LC39B
2006 Jul 4.78
12.77 days
2006 Jul 17.55
Delta wing
121485
37.5 long
5.5 dia
23.8 span
2006
2006
2006
2006
2006
2006
2006
2006
2006
4.80
5.71
6.15
6.50
6.76
14.63
16.04
17.42
17.49
51.63
51.63
51.63
51.63
51.64
51.63
51.63
51.63
51.63
88.35
88.65
90.40
91.35
91.37
91.35
91.35
91.35
91.35
6571
6586
6673
6720
6720
6719
6720
6719
6719
155
158
252
334
333
333
334
332
332
231
257
336
348
349
348
348
350
350
0.006
0.008
0.006
0.001
0.001
0.001
0.001
0.001
0.001
342
3
155
46
45
76
82
85
89
Genesis-1 %
[Dnepr]
2006-29 A
[29252]
YAS
2006 Jul 12.54
Inflatable
cyl+ 2 panels
1300
4.5 long
2.4 dia
2006 Jul 12.68
64.51
95.82 6937
555
561
0.0005
173
Dnper 2nd stage
2006-29 B
[29253]
2006 Jul 12.54
2006 Jul 12.61
2006 Jul 12.94
64.52
64.51
95.45 6919
95.53 6923
525
533
555
556
0.002
0.002
301
288
Fragment
2006-29
2006-29
2006-29
2006-29
[29256]
[31391]
[31392]
[35413]
2006 Jul 13.96
2007 May 7.10
2007 May 9.06
64.58
64.50
64.50
108.03 7515
95.52 6922
95.52 6922
540
521
521
1732
566
566
0.079
0.003
0.003
119
295
296
Cosmos 2422
(OKO)
[Molniya-M]
2006-30 A
[29260]
PLE
2006 Jul 21.18
2006 Jul 26.12
62.85
703.93 26213
533
39135
0.736
284
Molniya-M 4th stage 2006-30 B
Casing
[29261]
2006 Jul 21.18
2006 Aug 2.40
62.85
700.75 26134
537
38973
0.735
284
Molniya-M 3rd stage 2006-30 C
(Block I)
[29262]
2006 Jul 21.18
71 days
2006 Sep 30
2006 Jul 21.30
2006 Sep 30.92
62.83
62.81
91.47 6725
87.22 6515
228
133
464
141
0.017
0.0006
115
125
D
C
D
E
F
Cylinder
Jun
Jun
Feb
Apr
Nodal
period
(min)
4 dia
Jul
Jul
Jul
Jul
Jul
Jul
Jul
Jul
Jul
300
Cylinder
2000
8.1 long
2.66 dia
2006 30 continued on next page
** Crew of 7 astronauts (Lindsey, Kelly, Fossum, Nowak, Wilson, Sellers, Reiter) docked with ISS (Destiny/PMA-2 port) 2006 Jul 6.70. MPLM-1 Leonardo docked to
Destiny by station robotic arm for cargo transfer. Reiter remained onboard ISS with ISS Expedition 13/14; returned to earth with STS 116 2006 Dec 22.94,
171.36 days. Undocked 2006 Jul 15.42.
% 1/3 scale model of the Nautilus inflatable module.
$ Classified payload; # Target orbits from press kit; ## orbits from amateur observations
2014 - Version 1-13
RAE Table of Earth Satellites (extended)
(Compiled 2006)
Page 2006-11
Launchdate
Lifetime + Descent date
[Norad]
Shape and
weight (kg)
Descent date
Size
(m)
Lifetime
Date of
orbital
determination
Orbital
Inclination
(deg)
Semi
major axis
(km)
Year of Launch 2006
Name
[Launcher]
Fragments
Cospar ID
[Norad #] Launchsite
Cospar ID
Nodal
period
(min)
Perigee
height
(km)
Apogee
height
(km)
Orbital
Argument
eccentricity of perigee
(deg)
D
Molniya-M 4th stage 2006-30 D
(Block ML)
[29263]
2006 Jul 21.18
42 days
2006 Sep 1
Cylinder
900
2.3 long
2.2 dia
2006 Jul 21.30
2006 Sep 1.21
62.86
62.84
91.87 6745
87.62 6535
196
141
537
171
0.025
0.002
114
130
D
Fragments
2006-30 E
[29264]
2006 Sep 25
66 days
D
2006-30 F
[29266]
2006 Sep 2
43 days
D
2006-30 G
[29267]
2006 Sep 13
54 days
Kompsat 2 *
(Arirang 2)
[Rokot]
2006-31 A
[29268]
PLE-LC133
2006 Jul 28.30
Hexagonal
+ 2 panels
800
2.5 long
2 dia
6.8 span
2006
2006
2006
2006
2006
2006
2006
21.68
25.19
22.77
2.15
21.70
10.66
28.35
62.86
62.85
62.85
62.85
62.85
62.84
98.14
92.18
87.63
92.02
89.12
92.08
89.18
98.57
6760
6536
6752
6609
6755
6612
7069
226
149
213
183
220
194
679
537
165
533
278
533
273
701
0.023
0.001
0.024
0.007
0.023
0.006
0.002
116
103
117
122
115
129
222
Rokot 3rd stage
(Breeze KM)
2006-31 B
[29269]
2006 Jul 28.30
Cylinder
1700?
3 long
2.5 dia
2006 Jul 28.42
98.19
96.73 6980
504
700
0.014
249
Hotbird 8
[Proton-K]
2006-32 A
2006 Aug 4.99
[29270]
> million years
BAI-LC200/39
2006
2006
2006
2006
2006
49.11
13.04
0.11
0.11
0.10
414
3853
35770
35769
35782
35834
35804
35784
35803
35790
0.723
0.610
0.0002
0.0004
0.0001
0
0
21
43
86
Box+ 2 panels
4875
45 span
Aug
Aug
Aug
Aug
Aug
5.06
5.53
16.20
16.88
23.94
636.17
703.70
1435.63
1436.08
1436.08
24503
26207
42156
42165
42165
Proton-M 4th stage 2006-32 B
(Breeze-M)
[29254]
2006 Aug 4.99
Cylinder
1220
2.62 long
2.4 dia
2006 Aug 5.53
13.12
696.20 26021
3746
35539
0.611
0
Breeze-M APT #
2006 Aug 4.99
Torus
1290
2.1 long
4.1 dia
0.8 cross
2006 Sep 2.55
49.48
297.27 14755
310
16442
0.547
11
JCSAT 10
2006-33 A
[Ariane-5 ECA L531] [29272]
(V 172)
KOU-ELA3
2006 Aug 11.93
Box+ 2 panels
4048 full
1858 empty
5.5x2.2
x2.2
26.9 span
2006
2006
2006
2006
2006
2006
12.17
15.21
16.85
21.40
23.50
4.29
5.44
2.53
0.74
0.05
0.02
0.05
630.70
776.67
1077.33
1433.50
1435.27
1436.10
24362
27989
34812
42114
42149
42165
266
7481
21129
35710
35751
35781
35701
35739
35738
35761
35788
35791
0.727
0.505
0.210
0.0006
0.0004
0.0001
178
179
177
93
161
188
Syracuse 3B
2006-33 B
[29273]
2006 Aug 11.93
Box+ 2 panels
3750 full
1658 empty
4.0x2.3
x1.8
29.5 span
2006 Aug 12.59
2006 Aug 16.83
2006 Sep 9.16
6.01
0.00
0.05
628.10 24295
1436.03 42164
1436.10 42165
255
35770
35777
35577
35800
35796
0.727
0.0003
0.0002
181
55
241
Ariane-5 2nd stage
+ VEB
2006-33 C
[29274]
2006 Aug 11.93
Drum-cone
2880
Cylinder
950
3.5 long
3.94 dia
1.13 high
3.94 dia
2006 Aug 12.17
5.44
631.42 24381
264
35740
0.728
178
2006-32 C
[29271]
2006 33 continued on next page
#
Jul
Sep
Jul
Sep
Jul
Sep
Jul
Additional propellant tank, jettisoned after 4th burn.
2014 - Version 1-13
Aug
Aug
Aug
Aug
Aug
Sep
RAE Table of Earth Satellites (extended)
(Compiled 2006)
Page 2006-12
Launchdate
Lifetime + Descent date
[Norad]
Shape and
weight (kg)
Descent date
Semi
major axis
(km)
Year of Launch 2006
Name
[Launcher]
Fragments
D
Cospar ID
[Norad #] Launchsite
Cospar ID
Size
(m)
Lifetime
Date of
orbital
determination
Orbital
Inclination
(deg)
Nodal
period
(min)
Perigee
height
(km)
Apogee
height
(km)
Orbital
Argument
eccentricity of perigee
(deg)
270
35783
0.728
178
Sylda upperpart
2006-33 D
[29275]
2006 Aug 11.93
Barrel shaped
500?
2006 Aug 12.17
5.45
632.38 24405
Koreasat 5 *
(Mugunghwa 5)
[Zenit-3SL]
2006-34 A
[29349]
ODS
2006 Aug 22.14
Box+ 2 panels
4465
2006 Aug 22.64
2006 Aug 26.80
2006 Sep 9.69
0.06
0.04
0.06
679.08 25593
1434.00 42124
1436.10 42165
2900
35709
35780
35528
35781
35792
0.637
0.0009
0.0001
338
173
182
Zenit-3SL 3rd stage 2006-34 B
(Block-DM SL)
[29350]
2006 Aug 22.14
Cylinder
2140
2006 Aug 22.64
0.04
678.78 25585
2899
35514
0.637
304
SJ 8 $
[CZ-2C]
2006-35 A
[29385]
JIUQ
2006 Sep 9.29
53 days
2006 Nov 1
2006 Sep 9.40
62.99
90.75 6690
177
445
0.020
145
2006 Nov 1.82
62.97
87.13 6511
124
139
0.001
152
2006 Sep 9.40
2006 Oct 2.88
62.99
62.96
90.77 6691
87.62 6535
179
139
445
174
0.020
0.003
144
141
0.004
0.002
0.001
186
21
4
No elements available; orbit from amateur observations.
2007 Apr 7.01
97.34
94.35 6866
486
489
0.0002
99
2006 Oct 12.93
0.004
283
6.22 long
3.7 dia
D
CZ-2C 2nd stage
2006-35 B
[29386]
2006 Sep 9.29
24 days
2006 Oct 3
D
Fragments
2006-35 C-G
5 pieces, all have decayed
D STS 115 *
6M Atlantis F27
R
2006-36 A
[29391]
CC-LC39B
2006 Sep 9.63
11.63 days
2006 Sep 21.26
IGS-O 2 #
[H-2A]
2006-37 A
[29393]
TAN
2006 Sep 11.19
H-2A 2nd stage
2006-37 B
[29394]
2006 Sep 11.19
Fragments
2006-37 C-AA 12 pieces, all have decayed
For orbital information see extra pages at end of year
Zhing Xong 22A
(Chinasat 22A)
[CZ-3A]
2006-38 A
[29398]
XI
2006 Sep 12.67
> million years
2006 Sep 12.94
2006 Sep 19.60
2006 Oct 5.44
25.00
0.34
0.39
751.78 27388
1436.58 42175
1436.13 42166
D
CZ-3A 3rd stage
2006-38 B
[29399]
2006 Sep 12.67
57 days
2006 Nov 8
2006 Sep 12.95
2006 Nov 8.80
25.34
25.06
754.73 27460
90.12 6659
*
$
*
South Korean earth observing satellite.
A capsule with seeds was recovered 2006 Sep 24.11 in Sichuan province.
Crew of 6 astronauts (Jett, Ferguson, Burbank, Tanner, MacLean and Stefanyshyn-Piper) docked with ISS (front port of Destiny/PMA-2) 2006 Sep 11.45
They installed the P3/P4 portside truss and solar arrays. Undocked 2006 Sep 17.53
3rd Information Gathering Satellite Optical (IGS-2 lost in 2003 Nov launch failure).
D
#
2014 - Version 1-13
Cylinder
3400?
Delta wing
121485
Cylinder
3100
Cylinder
3060
11 long
3.35 dia
For orbital information see extra pages at end of year
37.5 long
5.5 dia
23.8 span
9.2 long
4 dia
12.38 long
3.0 dia
2006 Sep 9.66
2006 Sep 9.92
2006 Sep 21.16
51.63
51.64
51.63
97.23
89.63 6635
90.50 6678
91.38 6721
93.85 6841
228
285
334
433
284
314
350
492
202
35758
35758
41817
35834
35816
0.760
0.0009
0.0007
180
101
87
167
83
41995
477
0.762
0.296
180
229
Year of Launch 2006
Name
[Launcher]
Fragments
D
Cospar ID
[Norad #] Launchsite
Cospar ID
D
%
*
RAE Table of Earth Satellites (extended)
(Compiled 2006)
Page 2006-13
Shape and
weight (kg)
Descent date
Semi
major axis
(km)
Size
(m)
Lifetime
Date of
orbital
determination
Orbital
Inclination
(deg)
Perigee
height
(km)
Apogee
height
(km)
Orbital
Argument
eccentricity of perigee
(deg)
2006-39 A
[29402]
BAI-LC31
2006 Sep 14.57
70 days
2006 Nov 23
2006
2006
2006
2006
14.63
15.88
16.02
17.75
64.94
64.95
64.89
64.89
89.38
89.90
89.95
89.37
6622
6648
6651
6621
170
207
211
202
317
332
333
284
0.011
0.009
0.009
0.006
66
53
67
107
Soyuz 3rd stage
2006-39 B
[29403]
2006 Sep 14.57
2006 Sep 14.63
64.91
89.28 6618
166
312
0.011
66
Fragments
2006-39 C-AG 31 pieces, 30 have decayed
2006-40 A
[29400]
BAI-LC1
Sep
Sep
Sep
Nov
Nodal
period
(min)
Cosmos 2423 %
[Soyuz]
D Soyuz-TMA 9 *
3M [Soyuz-FG]
R
D
Launchdate
Lifetime + Descent date
[Norad]
For orbital information see extra pages at end of year
2006 Sep 18.17
215.35 days
2007 Apr 20.567
Cyl+ 2 panels+ 7.5 long
2006 Sep 18.93
beehive+sphere 2.3 to
2006 Sep 20.54
7250
2.72 maxdia 2007 Apr 20.38
51.63
51.63
51.63
89.38 6622
91.37 6720
91.18 6711
233
334
322
254
349
343
0.002
0.001
0.002
349
7
88
Soyuz-FG 3rd stage 2006-40 B
(Block I)
[29401]
2006 Sep 18.17
3 days
2006 Sep 21
Cylinder
2400?
2006 Sep 20.56
2006 Sep 20.86
51.65
51.65
87.80 6544
87.45 6527
161
146
170
150
0.0007
0.0003
39
1
Solar-B (Hinode)
[M-5 #17]
2006-41 A
[29479]
KAG
2006 Sep 22.90
2006 Sep 22.94
2006 Sep 24.18
98.31
98.31
94.10 6853
94.12 6855
271
281
678
671
0.030
0.028
131
126
M-5 3rd stage
2006-41 B
[29480]
2006 Sep 22.90
2006 Sep 23.79
98.35
94.02 6849
280
661
0.028
127
SSSAT?
2006-41 D
[29482]
2006 Sep 22.90
3 days
2006 Sep 25
2006 Sep 22.94
2006 Sep 24.82
98.32
98.30
93.95 6847
92.58 6780
278
269
658
534
0.028
0.020
130
115
HITSat
2006-41 F
[29484]
2006 Sep 22.90
2006 Sep 25.69
98.33
94.07 6852
279
668
0.028
120
Fragments
2006-41 C, E, G-L
7 pieces, 6 have decayed
8.1 long
2.66 dia
For orbital information see extra pages at end of year
Destroyed in orbit 2006 Nov 17 at the end of its mission.
Crew of 3 astronauts (ISS-Expedition 14: Lopez Alegria, Tyurin and space-participant Ansari) docked with the ISS (Zvezda aft port) 2006 Sep 20.06;
Ansari returned with Expedition-13 crew in Soyuz-TMA-8. Soyuz-TMA 9 undocked from Zvezda 2006 Oct 10.80 and redocked to Zarya 2006 Oct 10.82; undocked
2007 Mar 27.938 and redocked to Zvezda aft port 2007 Mar 27.954 with Lopez Alegria, Tyurin and Williams.
Soyuz-TMA 9 with Lopez Alegria, Tyurin and space-participant Simonyi (launched with Soyuz-TMA 10) undocked 2007 Apr 21.383 and landed in Kazachstan.
2014 - Version 1-13
RAE Table of Earth Satellites (extended)
(Compiled 2006)
Page 2006-14
Launchdate
Lifetime + Descent date
[Norad]
Shape and
weight (kg)
Descent date
Size
(m)
Lifetime
Semi
major axis
(km)
GPS IIR-15 (M2)
2006-42 A
[Delta-2(7925-9.5)] [29486]
CC-LC17A
2006 Sep 25.78
1 million years
Box+ 2 panels
2064
1.52 x 1.52 2006 Sep 25.83
x 1.93
2006 Sep 28.18
19.3 span
2006 Oct 8.16
39.94
54.93
54.94
D
Delta-2 3rd stage
(Star 48B)
2006-42 B
[29487]
Cone-cyl
205
2.29 long
1.50 dia
2006 Sep 25.83
2013 Dec 26.87
D
Delta-2 2nd stage
(Centaur)
2006-42 C
[29488]
2006 Sep 25.78
2650 days
2013 Dec 27
2006 Sep 25.78
89 days
2006 Dec 23
Cylinder
919
5.88 long
2.44 dia
Fragment
2006-42 D
Year of Launch 2006
Name
[Launcher]
Fragments
Cospar ID
[Norad #] Launchsite
Cospar ID
[38674]
Date of
orbital
determination
Orbital
Inclination
(deg)
Nodal
period
(min)
Perigee
height
(km)
Apogee
height
(km)
Orbital
Argument
eccentricity of perigee
(deg)
357.00 16670
725.28 26740
716.92 26559
174
20252
20019
20410
20471
20342
0.607
0.004
0.006
16
196
277
39.94
39.65
356.65 16659
88.65 6586
183
115
20378
299
0.606
0.014
16
152
2006 Sep 26.72
2006 Nov 11.91
2006 Dec 23.36
33.65
33.64
33.63
98.78 7079
95.52 6922
87.77 6543
183
172
131
1218
914
197
0.073
0.054
0.005
18
68
120
2012 Jul 15.60
39.91
294.12 14651
183
16361
0.552
196
DirecTV 9S
2006-43 A
[Ariane-5 ECA 533] [29494]
(V175)
KOU-ELA3
2006 Oct 13.87
> million years
Box+ 2 panels
5535 full
7.5x2.9x3.3 2006 Oct
31.3 span
2006 Oct
2006 Oct
2006 Oct
2006 Oct
2006 Oct
2006 Nov
2006 Nov
2006 Dec
14.12
18.27
21.31
22.42
25.59
27.10
8.97
12.47
12.47
7.01
0.14
0.04
0.04
0.03
0.03
0.06
0.05
0.02
632.00
1385.45
1436.60
1435.63
1434.05
1436.13
1433.25
1432.03
1436.08
24395
41168
42175
42156
42125
42166
42109
42085
42165
247
33774
35736
35732
35731
35760
35717
35695
35774
35786
35803
35856
35823
35761
35813
35743
35718
35798
0.728
0.025
0.001
0.001
0.0004
0.0006
0.0003
0.0003
0.0003
179
175
88
100
100
264
183
335
155
Optus D1
2006-43 B
[29495]
2006 Oct 13.87
> million years
Box+ 2 panels
2299 full
4.0x3.2x2.3 2006 Oct
17 span
2006 Oct
2006 Oct
2006 Oct
2006 Nov
2006 Nov
14.11
17.70
21.47
27.36
7.55
12.62
6.98
4.86
0.07
0.05
0.02
0.04
632.65
687.20
1433.30
1436.05
1441.08
1436.12
24412
25796
42110
42164
42262
42165
253
3062
35686
35777
35881
35773
35814
35773
35777
35793
35887
35800
0.728
0.634
0.001
0.0002
0.00007
0.0003
178
180
253
103
147
156
Sylda upper part
2006-43 C
[29496]
2006 Oct 13.87
Barrel shaped
500?
2006 Oct 14.05
2008 Jul 11.94
6.96
7.33
631.98 24395
104.60 7354
248
139
35786
1812
0.728
0.114
178
27
Ariane-5 2nd stage 2006-43 D
(+ LDREX-2) *
[29497]
2006 Oct 13.87
Drum-cone
2880
2006 Oct 13.96
6.97
632.83 24417
257
35819
0.728
178
Fragment
2006-43 E
[29498]
2006 Oct 14.04
6.91
629.53 34332
224
35683
0.729
177
MetOp A
[Soyuz-ST 2.1A]
2006-44 A
[29499]
BAI-LC31
2006 Oct 19.69
Box+ panel
4093 full
6.3x2.5x2.5 2006 Oct 19.75
8x5 panel
17.6 span
98.73
101.40 7203
824
826
0.0002
341
D
Soyuz-ST 4th stage
(Fregat 1011)
2006-44 B
[29500]
2006 Oct 19.69
< 1 day
2006 Oct 19
Spheres +
nozzle
1100?
1.5 high
3.3 dia
98.74
93.82 6839
99
822
0.053
245
*
Secondary Japanese payload, remained attached to 2nd stage. Large Deployable Reflector Experiment is a half-scale model of the antenna to be used on ETS-8.
The 0.7x0.6x1.9 payload has a mass of 211 kg and spans 6.5 m when deployed. After deployment the antenna was ejected.
D
2014 - Version 1-13
3.5 long
3.94 dia
2006 Apr 19.75
RAE Table of Earth Satellites (extended)
(Compiled 2006)
Page 2006-15
Launchdate
Lifetime + Descent date
[Norad]
Shape and
weight (kg)
Descent date
Semi
major axis
(km)
Year of Launch 2006
Name
[Launcher]
Fragments
Cospar ID
[Norad #] Launchsite
Cospar ID
Size
(m)
Lifetime
Date of
orbital
determination
Orbital
Inclination
(deg)
Nodal
period
(min)
Perigee
height
(km)
Apogee
height
(km)
Orbital
Argument
eccentricity of perigee
(deg)
D
Progress-M 58 #
[Soyuz-U]
2006-45 A
[29503]
BAI-LC1
2006 Oct 23.57
155.40 days
2007 Mar 27.972
Cyl+ 2 panels+ 7.9 long
2006 Oct 23.75
beehive+sphere 2.12 maxdia 2006 Oct 26.60
7265
2007 Mar 27.45
51.64
51.63
51.63
89.25 6616
91.28 6716
91.25 6714
234
329
325
240
346
349
0.0005
0.001
0.002
70
138
358
D
Soyuz-U 3rd stage
(Block I)
2006-45 B
[29504]
2006 Oct 23.57
4 days
2006 Oct 27
Cylinder
2400?
8.1 long
2.66 dia
2006 Oct 23.57
2006 Oct 25.84
2006 Oct 27.37
51.57
51.63
51.61
88.68 6588
88.38 6573
87.43 6526
199
179
144
219
210
151
0.001
0.002
0.0005
79
49
45
Shijian 6-2A
[CZ-4B2]
2006-46 A
[29505]
TAI
2006 Oct 23
Cube
+ 2 panels
375?
1 side
4 span
2006 Oct 24.03
97.71
96.70 6979
592
608
0.001
75
Shijian 6-2B
2006-46 B
[29506]
2006 Oct 23
Cube
+ 2 panels
975?
1.4 side
8.6 span
2006 Oct 24.16
2006 Oct 24.77
97.67
97.71
96.50 6970
96.65 6977
560
596
622
601
0.004
0.0004
290
83
CZ-4B2 3rd stage
2006-46 C
[29507]
2006 Oct 23
Cylinder
1727
4.93 long
2.9 dia
2006 Oct 24.09
97.71
96.60 6974
591
601
0.0007
98
Fragments
2006-46 D-L
8 pieces, 1 has decayed
For orbital information see extra pages at end of year
AHEAD (Stereo A) $ 2006-47 A
[Delta-2 7925-10L] [29510]
CC-LC17B
2006 Oct 26.04
Indefinitely
2006 Oct 26
2006 Dec 15
Solar orbit
28.5
33.6
0.12
BEHIND (Stereo B)$$ 2006-47 B
[29511]
2006 Oct 26.04
Indefinitely
2006 Oct 26
2006 Dec 15
Solar orbit
0.185
0.006
148
37
0.191
150
344 days
182
403810
180000 1750000
0.95
0.97
28.5
27.9
0.03
389 days
182
403810
130000 870000
0.99
1.09
119.73 8047
87.90 6549
184
133
3154
208
182
403810
85
3148
D
Delta-2 2nd stage
2006-47 C
[29512]
2006 Oct 26.04
371 days
2007 Nov 1
2006 Oct 26.27
2007 Oct 31.82
24.58
24.48
D
Delta-2 3rd stage
Star-48B
2006-47
[NNN]
2006 Oct 26.04
10 days
2006 Nov 6
2006 Oct 26
28.5
D
Fragment
2006-47 D
[29513]
2006 Oct 26.10
28.44
#
2006 Oct 26
< 1 day
118.57 7995
Soft-docked with ISS (Zvezda aft port) 2006 Oct 26.44; hard-docking 2006 Oct 26.75 due to a possible problem with a Kurs antenna. Antenna freed by spaceWalking astronauts. Undocked 2007 Mar 27.756 and de-orbited over Pacific Ocean.
$ By using Moon gravity assist (2006 Dec 15 at 5937 km) AHEAD will go to a position about 1 million km ahead of Earth in its orbit around the sun.
$$ By using two Moon gravity assists (2006 Dec 15 at 10746 km and 2007 Jan 21 at 16029 km) BEHIND will go to a position about 1 million km behind Earth in
its orbit around the sun.
2014 - Version 1-13
Year of Launch 2006
Name
[Launcher]
Fragments
D
Cospar ID
[Norad #] Launchsite
Cospar ID
Launchdate
Lifetime + Descent date
[Norad]
RAE Table of Earth Satellites (extended)
(Compiled 2006)
Page 2006-16
Shape and
weight (kg)
Descent date
Semi
major axis
(km)
Size
(m)
Lifetime
Date of
orbital
determination
Orbital
Inclination
(deg)
Orbital
Argument
eccentricity of perigee
(deg)
3372
11562
35468
35682
35660
35671
35827
35880
35784
35896
35899
35909
0.625
0.404
0.004
0.003
0.003
0.003
181
184
214
145
147
146
186
142
35797
33383
0.731
0.718
181
239
1256
15049
35499
35782
35854
35782
36014
36040
36084
35790
35981
35789
0.695
0.329
0.007
0.00009
0.002
0.00008
15
23
183
158
74
240
2006 Oct 28
> million years
2006
2006
2006
2006
2006
2007
30.32
31.36
2.37
5.48
5.85
29.77
18.11
6.64
0.02
0.37
0.36
0.17
CZ-3B 3rd stage
2006-48 B
[29517]
2006 Oct 28
2006 Oct 30.66
2007 Jan 30.63
28.70
28.34
XM 4 (Blues)
[Zenit-3 SL]
2006-49 A
[29520]
ODS
2006 Oct 30.99
> million years
2006
2006
2006
2006
2006
2006
31.02
6.81
13.16
27.76
12.35
19.30
0.07
0.16
0.07
0.03
0.01
0.03
2006 Oct 31.02
0.00
656.85 25031
1263
36041
0.695
221
2006 Nov 6.68
98.79
101.88 7226
841
854
0.0009
257
2006 Nov 4.63
98.79
101.85 7225
830
862
0.002
241
Zenit-3SL 3rd stage 2006-49 B
(Block DM-SL)
[29521]
2006 Oct 30.99
DMSP 5D-3 F17
[Delta 4 Medium]
2006-50 A
[29522]
VDB-SLC6
2006 Nov 4.58
Delta 4 2nd stage * 2006-50 B
[29523]
2006 Nov 4.58
0.06 days
2006 Nov 4.66
Cylinder
2140
6.22 long
3.7 maxdia
25978
30100
42005
42167
42158
42168
Apogee
height
(km)
2006-48 A
[29516]
XI
Oct
Nov
Nov
Nov
Dec
Dec
694.48
866.17
1427.93
1436.23
1435.77
1436.27
Perigee
height
(km)
Sinosat 2 #
[CZ-3B]
5193
Oct
Oct
Nov
Nov
Nov
Jan
Nodal
period
(min)
631.02 24370
583.88 23141
656.17
946.03
1436.35
1436.08
1442.80
1436.08
25014
31923
42170
42164
42296
42165
1200
Fragments **
2006-50 C-BX 68 pieces, 5 have decayed
For orbital information see extra pages at end of year
Arabsat 4B
(Badr 4)
[Proton-M]
2006-51 A
2006 Nov 8.83
[29526]
> million years
BAI-LC200/39
2006
2006
2006
2006
Box+ 2 panels
3304 full
1487 dry
Nov
Nov
Nov
Nov
8.84
8.88
16.68
21.64
51.53
14.13
0.08
0.07
87.98
688.87
1431.05
1436.07
6553
25838
42066
42164
174
3141
35593
35763
175
35777
35782
35808
0.0001
0.632
0.002
0.0005
270
0
75
332
Proton-M 4th stage 2006-51 B
(Breeze-M)
[29527]
2006 Nov 8.83
Cylinder
1220
2.62 long
2.4 dia
2006 Nov 8.88
14.23
689.73 25859
3164
35797
0.631
0
Breeze-M APT
2006 Nov 8.83
Torus
1290
2.1 long
4.1 dia
0.8 cross
2006 Nov 9.44
51.50
395.37 17844
672
22259
0.605
12
#
*
2006-51 C
[29528]
Solar arrays didn’t deploy completely; satellite considered a loss.
Delta 4 Medium 2nd stage made a 3 minute depletion burn that resulted in de-orbiting the stage. However a large number of debris was tracked;
it possibly was generated around the time of the de-orbit burn.
** Fragments C and D are the two instrument covers of the Operational Linescan System.
2014 - Version 1-13
RAE Table of Earth Satellites (extended)
(Compiled 2006)
Page 2006-17
Launchdate
Lifetime + Descent date
[Norad]
Shape and
weight (kg)
Descent date
Size
(m)
Lifetime
Semi
major axis
(km)
GPS IIR-16 (M3)
2006-52 A
[Delta-2(7925-9.5)] [29601]
CC-LC17A
2006 Nov 17.80
1 million years
Box+ 2 panels
2064
1.52 x 1.52 2006 Nov 17.84
x 1.93
2006 Nov 19.27
19.3 span
39.96
55.05
Delta-2 2nd stage
(Centaur)
2006-52 B
[29602]
2006 Nov 17.80
Cylinder
919
5.88 long
2.44 dia
2006 Nov 18.34
Delta-2 3rd stage
(Star 48B)
2006-52 C
[29603]
2006 Nov 17.80
170 days
2007 May 6
Cone-cyl
205
2.29 long
1.50 dia
Fragment
2006-52 D
Feng Yun 2D
[CZ-3A]
Year of Launch 2006
Name
[Launcher]
Fragments
D
Cospar ID
[Norad #] Launchsite
Cospar ID
Perigee
height
(km)
Apogee
height
(km)
Orbital
Argument
eccentricity of perigee
(deg)
356.05 16641
722.10 26662
188
20205
20336
20362
0.605
0.003
16
246
39.95
356.40 16652
188
20357
0.606
16
2006 Nov 17.91
2007 May 6.36
32.67
32.62
98.93 7086
87.60 6534
192
137
1223
174
0.073
0.003
11
225
[38675]
2012 Jul
39.96
175.43 10381
160
7845
0.370
22
2006-53 A
[29640]
XI
2006 Dec 8.04
> million years
2006
2006
2006
2006
CZ-3A 3rd stage
2006-53 B
[29641]
2006 Dec 8.04
> million years
Fragment
2006-53 C
2006-53 D
WildBlue 1
[Ariane-5 ECA]
Americom 18
16.89
24597
42397
42165
42166
230
35786
35775
35781
36208
36250
35797
35794
0.731
0.005
0.0003
0.0002
180
32
104
147
2006 Dec 9.26
2.63
1456.73 42568
35891
36488
0.007
27
[29642]
[33458]
2006 Dec 9.27
2008 Dec 14.52
2.70
0.75
1449.58 42429
1436.05 42164
35599
35581
36501
35989
0.011
0.005
40
331
2006-54 A
[29643]
KOU-ELA3
2006 Dec 8.92
> million years
2006 Dec 9.60
2006 Dec 12.79
2006 Dec 26.56
2.01
0.06
0.05
632.05 24397
1391.37 41285
1436.10 42165
258
34036
35779
35778
35775
35793
0.728
0.021
0.0002
179
152
74
2006-54 B
[29644]
2006 Dec 8.92
> million years
2006
2006
2006
2006
2.01
0.14
0.03
0.04
631.27
1197.55
1435.63
1436.10
249
26202
35768
35784
35748
35753
35786
35788
0.728
0.128
0.0002
0.00005
179
166
249
105
2006 Dec 8.92
Drum-cone
2880
Sylda upperpart
2006 Dec 8.92
Barrel shaped
500?
2006-54 D
[29646]
12.38 long
3.0 dia
3.5 long
3.94 dia
Dec
Dec
Dec
Dec
8.17
12.61
18.00
18.79
Nodal
period
(min)
639.87
1447.97
1436.08
1436.17
Cylinder
3060
Dec
Dec
Dec
Dec
Orbital
Inclination
(deg)
24.87
2.63
2.61
2.61
Ariane-5 2nd stage 2006-54 C
[29645]
2014 - Version 1-13
Date of
orbital
determination
10.04
12.15
18.80
22.40
24377
37356
42156
42165
2006 Dec 9.14
2.04
631.18 24374
259
35732
0.728
182
2006 Dec 9.60
2.01
631.58 24385
259
35754
0.728
179
RAE Table of Earth Satellites (extended)
(Compiled 2006)
Page 2006-18
Launchdate
Lifetime + Descent date
[Norad]
Shape and
weight (kg)
Descent date
Size
(m)
Lifetime
Date of
orbital
determination
Orbital
Inclination
(deg)
Semi
major axis
(km)
Year of Launch 2006
Name
[Launcher]
Fragments
Cospar ID
[Norad #] Launchsite
Cospar ID
Perigee
height
(km)
Apogee
height
(km)
Orbital
Argument
eccentricity of perigee
(deg)
D STS-116 #
7M Discovery F33
R [Shuttle]
2006-55 A
[29647]
CC-LC39B
2006 Dec 10.07
12.87 days
2006 Dec 22.94
Delta wing
37.5 long
5.5 dia
23.8 span
2006
2006
2006
2006
2006
2006
2006
2006
2006
10.10
10.27
11.15
11.99
19.58
19.98
20.01
22.03
22.64
51.63
51.64
51.64
51.63
51.64
51.63
51.64
51.63
51.63
89.25
90.35
90.93
91.38
91.37
91.25
91.05
91.07
91.05
6616
6670
6699
6721
6720
6714
6705
6705
6705
225
247
297
326
325
316
315
314
313
250
336
344
358
357
356
336
339
339
0.002
0.007
0.003
0.002
0.002
0.003
0.002
0.002
0.002
207
332
13
325
353
354
3
16
19
D
MEPSI 2A+2B $
2006-55 B
[29660]
2006 Dec 10.07
88 days
2007 Mar 8
Cube
3.5 together
0.10x0.10
x0.125
2006 Dec 21.24
2007 Feb 1.38
2007 Mar 8.77
51.64
51.63
51.61
90.95 6700
90.37 6671
87.27 6518
311
288
135
332
297
144
0.002
0.0007
0.0007
28
163
308
D
RAFT $$
2006-55 C
[29661]
2006 Dec 10.07
171 days
2007 May 30
Cube
4
0.125x0.125 2006 Dec 21.17
x0.125
2007 May 30.06
51.65
51.62
90.97 6701
87.15 6512
313
129
332
138
0.001
0.0007
17
191
D
MARSCom $$
2006-55 D
[29662]
2006 Dec 10.07
147 days
2007 May 6
Cube
3
0.125x0.125 2006 Dec 21.78
x0.125
2007 May 6.40
51.64
51.61
90.98 6702
87.37 6523
313
141
333
147
0.002
0.0004
345
252
D
ANDE Cylinder 1 %
2006-55 E
[29663]
2006 Dec 10.07
129 days
2007 Apr 18
Cylinder
0.5 dia
2006 Dec 22.25
2007 Apr 17.81
51.64
51.64
91.02 6703
87.55 6531
312
151
336
154
0.002
0.0002
24
320
D
ANDE MAA Sphere 1* 2006-55 F
[29664]
2006 Dec 10.07
380 days
2007 Dec 25
Sphere
50
0.483 dia
2006 Dec 22.92
2007 Dec 25.17
51.63
51.62
91.02 6703
87.18 6513
312
132
337
137
0.002
0.0003
19
249
D
ANDE Cylinder 2 %
2006-55 G
[29665]
2006 Dec 10.07
61 days
2007 Feb 9
Cylinder
0.5 dia
2006 Dec 22.98
2007 Jan 10.58
2007 Feb 9.47
51.64
51.63
51.62
91.02 6703
90.60 6683
87.62 6535
312
297
155
336
311
158
0.002
0.001
0.0002
21
91
159
D
ANDE Avionics Deck& 2006-55 H
[29666]
2006 Dec 10.07
135 days
2007 Apr 24
Disc
0.5 dia
2006 Dec 22.98
2007 Apr 24.28
51.64
51.60
91.02 6703
87.70 6539
312
158
336
163
0.002
0.0004
21
280
ANDE FCal Sphere 2* 2006-55 J
[29667]
2006 Dec 10.07
Sphere
+ 4 antennae
25
0.445 dia
2006 Dec 22.98
51.64
91.02 6703
312
336
0.002
22
#
Dec
Dec
Dec
Dec
Dec
Dec
Dec
Dec
Dec
Nodal
period
(min)
Crew of 7 astronauts (Polansky, Oefelein, Curbeam, Patrick, Fuglesang, Higginbotham and Williams) docked with ISS (Destiny front port) 2006 Dec 11.93;
undocked 2006 Dec 19.92. Williams stayed aboard ISS; Reiter returned with STS 116.
$ Micro Electro-Mechanical Systems-based PicoSat Inspector released from cargo bay 2006 Dec 20.03; two cube picosats with a 15.2 m tether.
$$ RAdar Fence Transponder + MARScom, two cubesats released from cargo bay 2006 Dec 20.12;
* Released 2006 Dec 21.77 from shuttle cargo bay. Atmospheric Neutral Density Experiment (ANDE) Risk Reduction flight consists of 2 small satellites: Mock
ANDE Active (MAA) and FenceCalibration (FCal). Nickel coated aluminium hollow spheres with laser retro reflectors. MAA also has 3 laser emitting diodes.
FCal has a radio transmitter. FCal didn’t deploy from its bus initially.
% Upper and lower bus that housed the satellites when deployed from shuttle cargo bay.
& Disc shaped intersection between Cylinder 1 and 2.
2014 - Version 1-13
Year of Launch 2006
Name
[Launcher]
Fragments
Cospar ID
[Norad #] Launchsite
Cospar ID
Launchdate
Lifetime + Descent date
[Norad]
RAE Table of Earth Satellites (extended)
(Compiled 2006)
Page 2006-19
Shape and
weight (kg)
Descent date
Semi
major axis
(km)
Size
(m)
Lifetime
Date of
orbital
determination
Orbital
Inclination
(deg)
2006
2006
2006
2006
12.13
14.20
22.75
26.58
49.07
16.81
2.00
0.08
Orbital
Argument
eccentricity of perigee
(deg)
416
7427
35331
35774
35806
35644
35477
35798
0.723
0.505
0.002
0.0003
0
0
0
305
2006 Dec 11.98
> million years
Breeze-M APT
2006-56 B
[29649]
2006 Dec 11.98
Torus
1290
2.1 long
4.1 dia
0.8 cross
2006 Dec 12.13
49.50
299.87 14840
320
16603
0.549
354
Proton-M 4th stage 2006-56 C
(Breeze-M 88518)
[29650]
2006 Dec 11.98
Cylinder
1220
2.62 long
2.4 dia
2006 Dec 12.62
16.59
776.52 27985
7454
35759
0.506
0
NRO-L 21 *
(USA 193)
[Delta-2 7920]
2006-57 A
[29651]
VDB-SLC-2W
2006 Dec 14.88
2006 Dec 16.25
2007 Jul 28.06
2008 Jan 22.27
58.49
58.49
58.49
91.83 6743
91.13 6709
90.05 6655
355
323
271
373
337
282
0.001
0.001
0.0008
82 #
77 #
84 #
Delta-2 2nd stage
(Centaur)
2006-57 B
[29652]
2006 Dec 14.88
Cylinder
919
5.88 long
2.44 dia
Delta-2 3rd stage
(Star 48B)
2006-57
[NNA]
2006 Dec 14.88
Cone-cyl
205
2.29 long
1.50 dia
Fragments **
2006-57 C-GH 174 pieces, 103 have decayed
For orbital information see extra pages at end of year
TacSat 2
[Minotaur 1]
2006-58 A
[29653]
WLI-LA0B
2006 Dec 16.50
Cylinder
+ 2 panels
370
2006 Dec 16.67
2006 Dec 17.21
40.01
40.01
92.93 6797
92.92 6796
414
409
422
425
0.0006
0.001
159
142
Genesat 1
2006-58 B
[29654]
2006 Dec 16.50
Box
3
2006 Dec 17.00
40.02
92.90 6795
413
420
0.0005
156
Minotaur-1
4th stage
2006-58 C
[29655]
2006 Dec 16.50
2006 Dec 17.00
40.02
92.88 6795
413
419
0.0004
149
ETS 8
[H-2A 204]
2006-59 A
[29656]
TAN
2006 Dec 18.27
2006
2006
2006
2007
18.52
19.40
23.89
16.69
28.49
16.80
1.04
0.11
252
4057
35801
35776
35991
35993
35866
35797
0.729
0.605
0.0008
0.0003
179
179
239
56
H-2A 2nd stage
2006-59 B
[29657]
2006 Dec 18.27
2006 Dec 20.20
28.52
268
34618
0.721
180
Box+ 2 panels
+ 2 dishes
5800
Cylinder
40 span
17x19
11.0 long
4.0 dia
Dec
Dec
Dec
Jan
636.07
701.62
1438.52
1436.10
24500
26404
42212
42165
609.85 23822
* USA-193 malfunctioned shortly after launch and stayed in low parking orbit.
** On 2008 Feb 21.143 USA-193 was hit by a Aegis-SM3 missile from warship USS Lake Erie west of Hawaii and destroyed.
# TLE derived from amateur visual observation.
2014 - Version 1-13
24490
27914
41783
42164
Apogee
height
(km)
2006-56 A
[29648]
BAI
0.10x0.10
x0.34
635.67
773.55
1416.62
1436.07
Perigee
height
(km)
MEASAT 3
[Proton-M 53521]
4765 full
3220 empty
Dec
Dec
Dec
Dec
Nodal
period
(min)
RAE Table of Earth Satellites (extended)
(Compiled 2006)
Page 2006-20
Launchdate
Lifetime + Descent date
[Norad]
Shape and
weight (kg)
Descent date
Semi
major axis
(km)
2006-60 A
[29658]
PLE
2006 Dec 19.58
Kosmos-3M 2nd stage 2006-60 B
[29659]
2006 Dec 19.58
Fragment
2006-60 C
Meridian 1
[Soyuz-2-1a]
Year of Launch 2006
Name
[Launcher]
Fragments
Cospar ID
[Norad #] Launchsite
Cospar ID
Date of
orbital
determination
Orbital
Inclination
(deg)
Box +
4x3x2
parabolic dish 3.3x2.7
770
2006 Dec 19.71
98.17
Cylinder
1434
2006 Dec 19.71
2006 Dec 22.74
[38844]
2006-61 A
[29668]
BAI
2006 Dec 24.36
Soyuz-FG 4th stage 2006-61 B
(Fregat)
[29669]
2006 Dec 24.36
SAR-Lupe 1
[Kosmos-3M
11K65M-SL]
Spheres
1100?
Size
(m)
Lifetime
4.22 long
2.4 to
3.2 maxdia
1.5 high
3.3 dia
Fragment
2006-61 C ? [29676]
(Listed as 2006-61 B by SpaceTrack)
Nodal
period
(min)
Perigee
height
(km)
Apogee
height
(km)
Orbital
Argument
eccentricity of perigee
(deg)
94.33 6865
467
505
0.003
175
98.16
98.16
94.33 6865
94.32 6864
464
460
508
510
0.003
0.004
169
151
2012 Sep 30.65
98.10
93.32 6815
418
455
0.003
335
2006 Dec 24.41
2006 Dec 24.90
2007 Jan 18.65
62.83
62.85
62.81
712.20 26418
727.38 26792
726.93 26781
278
1011
1030
39801
39815
39775
0.748
0.724
0.723
8
295
295
2006 Dec 25.92
2006 Dec 27.43
62.82
62.83
727.00 26783
726.47 26770
996
1031
39812
39751
0.725
0.723
295
295
2006 Dec 27.43
62.83
727.02 26783
997
39812
0.725
295
Cosmos 2425 *
[Proton-K 410-15/
Block DM-2 108L]
2006-62 A
[29670]
BAI-LC81/24
2006 Dec 25.85
Cyl+ 2 panels+ 2.4 dia
magnometerboom 3.7 height
1370
7.2 span
2006
2006
2007
2007
2007
2007
2007
2007
Dec
Dec
Jan
Jan
Jan
Jan
Feb
Feb
25.97
26.71
4.37
11.67
12.88
17.49
7.51
13.61
64.81
64.81
64.81
64.84
64.81
64.81
64.82
64.83
674.60
674.78
675.73
678.23
678.72
680.95
675.77
675.72
25480
25484
25508
25571
25583
25639
25509
25508
19072
19078
19123
19111
19139
19143
19065
19063
19130
19133
19137
19274
19270
19379
19196
19195
0.001
0.001
0.0003
0.003
0.003
0.005
0.003
0.003
204
213
307
52
54
68
348
346
Cosmos 2426 *
2006-62 B
[29671]
2006 Dec 25.85
Cyl+ 2 panels+ 2.4 dia
magnometerboom 3.7 height
1370
7.2 span
2006
2007
2007
2007
Dec
Jan
Jan
Feb
26.44
11.59
14.22
10.50
64.82
64.83
64.84
64.85
676.40
673.92
672.07
675.72
25525
25463
25416
25508
19137
19031
18938
19079
19156
19137
19136
19180
0.0004
0.002
0.004
0.002
58
228
237
180
Cosmos 2424 *
2006-62 C
[29672]
2006 Dec 25.85
Cyl+ 2 panels+ 2.4 dia
magnometerboom 3.7 height
1370
7.2 span
2006
2007
2007
2007
Dec
Jan
Jan
Feb
26.44
12.52
16.60
3.47
64.80
64.81
64.83
64.83
675.73
678.73
680.75
675.72
25508
25584
25634
25508
19118
19133
19146
19086
19141
19277
19365
19173
0.0005
0.003
0.004
0.002
289
50
78
179
Proton-K 3rd stage 2006-62 D
(8S812)
[29673]
2006 Dec 25.85
Cylinder
4185
4 long
4.1 dia
2007 Jan 4.54
64.82
674.77 25484
19076
19135
0.001
213
D
Proton-K 4th stage 2006-62 E
Casing
[29674]
2006 Dec 25.85
1 day
2006 Dec 26
Hollow cyl
800?
4.0 long
3.7 dia
2006 Dec 26.21
2006 Dec 26.33
64.72
64.82
87.47 6527
87.13 6511
134
127
164
139
0.002
0.0009
198
244
*
Glonass payloads
2014 - Version 1-13
2006-62 continued on next page
RAE Table of Earth Satellites (extended)
(Compiled 2006)
Page 2006-21
Launchdate
Lifetime + Descent date
[Norad]
Shape and
weight (kg)
Descent date
Size
(m)
Lifetime
Date of
orbital
determination
Orbital
Inclination
(deg)
Semi
major axis
(km)
Proton-K 4th stage 2006-62 F
(Block DM-2)
[29675]
2006 Dec 25.85
1 day
2006 Dec 26
Cylinder
2350?
6.22 long
3.7 maxdia
2006 Dec 26.02
2006 Dec 26.27
2006 Dec 26.33
64.80
64.81
64.80
Proton-K
Ullage motor
2006-62 G
[29680]
2006 Dec 25.85
Cylinder
55
0.90 long
0.68 dia
2006 Dec 27.62
Proton-K
Ullage motor
2006-62 H
[29682]
2006 Dec 25.85
Cylinder
55
0.90 long
0.68 dia
CoRoT #
[Soyuz 2-1b]
2006-63 A
[29678]
BAI
2006 Dec 27.60
Box+tube
+ 2 panels
626
Soyuz 2-1b 3rd
stage (Fregat)
2006-63 B
[29679]
2006 Dec 27.60
Cylinder
2400?
Year of Launch 2006
Name
[Launcher]
Fragments
D
#
Cospar ID
[Norad #] Launchsite
Cospar ID
Nodal
period
(min)
Perigee
height
(km)
Apogee
height
(km)
Orbital
Argument
eccentricity of perigee
(deg)
87.35 6522
87.32 6520
87.28 6518
140
136
135
147
147
145
0.0005
0.0008
0.0008
75
8
132
64.85
340.28 16146
407
19127
0.580
193
2007 Jan 3.47
64.74
340.23 16144
405
13127
0.580
193
4.2 long
9 span
2006 Dec 27.66
90.03
103.00 7279
893
908
0.001
117
8.1 long
2.66 dia
2006 Dec 27.66
90.02
88.92 6600
215
227
0.0009
3
Convection Rotation and planetary Transits, an ESA satellite, will search for planets outside the solar system.
2014 - Version 1-13
RAE Table of Earth Satellites
Year of Launch 2006
Cospar ID
[Norad number]
Descent date
Lifetime
ALOS H-2A 2ND STAGE fragments; 23 pieces, 21 have decayed
D 2006-02 C
[29364]
2006 Dec 4
314 days
D 2006-02 D
[29365]
2006 Dec 12
322 days
D
2006-02 E
[29366]
2006 Nov 3
283 days
D
2006-02 F
[29367]
2006 Oct 18
267 days
D
2006-02 G
[29368]
2006 Oct 18
267 days
D
2006-02 H
[29369]
2006 Nov 25
305 days
D
2006-02 J
[29370]
2006 Nov 13
293 days
D
2006-02 K
[29371]
2006 Oct 26
275 days
D
2006-02 L
[29372]
2006 Nov 17
297 days
D
2006-02 M
[29373]
2006 Nov 22
302 days
D
2006-02 N
[29374]
2006 Nov 9
289 days
D
2006-02 P
[29375]
2007 Jan 8
349 days
D
2006-02 Q
[29376]
2006 Nov 20
300 days
D
2006-02 R
[29377]
2006 Oct 10
259 days
D
2006-02 S
[29378]
2006 Nov 23
303 days
D
2006-02 T
[29379]
2006 Nov 20
300 days
D
2006-02 U
[29380]
2007 Jan 9
351 days
D
2006-02 V
[29381]
2006 Oct 17
266 days
D
2006-02 W
[29382]
2006 Oct 14
263 days
D
2006-02 X
[29383]
2006 Nov 11
291 days
D
2006-02 Y
[29384]
2006 Oct 26
275 days
2006-02 Z
2006-02 AA
[35418]
[36571]
Arabsat 4A
2006-06
2006-06
2006-06
2006-06
2006-06
Breeze-M stage fragments; 101 pieces, 5 have decayed
C
[32025]
D
[32026]
E
[32027]
F
[32028]
G
[32029]
2014 - Version 1-13
(Compiled 2006)
Nodal
period
(min)
Extra Page 2006 -1
Date of
orbital
Determination
Orbital
Inclination
(deg)
Semi
major axis
(km)
2006
2006
2006
2006
2006
2006
2006
2006
2006
2006
2006
2006
2006
2006
2006
2006
2006
2006
2006
2006
2006
2006
2007
2006
2006
2006
2006
2006
2006
2006
2006
2006
2006
2006
2006
2006
2006
2006
2006
2006
2006
Sep
Sep
Dec
Sep
Nov
Sep
Oct
Sep
Oct
Sep
Nov
Sep
Nov
Sep
Oct
Sep
Nov
Sep
Nov
Sep
Nov
Sep
Jan
Sep
Nov
Sep
Oct
Sep
Nov
Sep
Nov
Sep
Oct
Sep
Oct
Sep
Sep
Sep
Nov
Sep
Oct
8.26
8.25
12.11
8.17
17.32
8.30
17.75
8.25
17.35
8.47
23.76
8.17
10.75
8.42
29.17
8.25
15.77
8.22
21.74
8.23
9.17
8.42
7.83
8.46
19.21
8.43
7.17
8.22
21.05
8.47
20.18
8.18
22.01
8.25
16.35
8.68
30.76
8.68
2.72
8.70
25.73
98.18
98.21
98.22
98.22
97.92
98.20
98.18
98.23
98.26
98.21
98.21
98.21
98.18
98.20
98.21
98.21
98.21
98.20
98.22
98.21
98.21
98.22
98.21
98.21
98.21
98.23
98.26
98.21
98.22
98.18
98.19
98.20
98.40
98.21
98.20
98.16
97.90
98.20
98.22
98.23
98.24
96.52
96.75
91.13
96.17
92.35
95.62
90.88
95.83
91.62
96.67
91.92
96.33
92.38
96.13
91.32
96.53
91.90
96.87
91.55
96.33
91.18
96.88
90.67
96.57
91.97
95.58
92.53
96.88
92.47
96.70
91.67
97.03
95.78
95.82
91.43
95.95
94.08
96.62
92.67
96.22
91.25
2007
2007
2007
2007
2007
Aug
Aug
Aug
Aug
Aug
15.80
15.83
15.62
14.44
14.16
51.68
51.22
51.37
51.77
51.59
275.38
263.85
265.28
283.65
276.42
Perigee
height
(km)
Apogee
height
(km)
Orbital
eccentric.
Argument
of perigee
(deg)
6970
6982
6709
6954
6768
6927
6696
6937
6733
6978
6747
6962
6770
6952
6717
6971
6746
6987
6729
6961
6711
6988
6686
6973
6750
6925
6777
6988
6774
6979
6734
6995
6935
6937
6724
6943
6853
6975
6784
6956
6715
528
536
320
529
382
462
292
482
311
520
346
501
293
494
311
509
348
547
334
502
312
526
294
517
355
466
377
546
375
531
339
543
530
477
319
504
397
538
377
508
320
655
670
340
621
397
634
343
635
397
678
391
666
489
653
366
677
387
670
367
663
353
693
321
671
387
627
421
672
416
670
372
691
583
639
371
624
552
654
433
648
352
0.009
0.010
0.002
0.007
0.001
0.012
0.004
0.011
0.006
0.011
0.003
0.012
0.014
0.011
0.004
0.012
0.003
0.009
0.002
0.012
0.003
0.012
0.002
0.011
0.002
0.012
0.003
0.009
0.003
0.010
0.002
0.011
0.004
0.012
0.004
0.009
0.011
0.008
0.004
0.010
0.002
127
131
230
126
285
101
301
104
297
120
274
114
122
113
278
120
258
121
289
114
290
118
334
120
284
107
328
124
209
116
280
157
115
109
300
120
248
118
254
110
274
14022
13627
13676
14301
14057
435
516
548
472
410
14851
13981
14047
15373
14946
0.514
0.494
0.494
0.521
0.517
293
302
300
289
293
RAE Table of Earth Satellites
Year of Launch 2006
Cospar ID
[Norad number]
Descent date
Lifetime
D
2006-06
2006-06
2006-06
2006-06
2006-06
2006-06
2006-06
2006-06
2006-06
2006-06
2006-06
2006-06
2006-06
2006-06
2006-06
2006-06
H
J
K
L
M
N
P
Q
R
S
T
U
V
W
X
Y
[32030]
[32031]
[32032]
[32033]
[32034]
[32035]
[32036]
[32037]
[32038]
[32039]
[32040]
[32041]
[32042]
[32043]
[32044]
[32045]
2008 Jan 4
675 days
D
2006-06 Z
[32046]
2008 Mar 2
733 days
2006-06
2006 06
2006 06
2006 06
2006 06
2006 06
2006 06
2006 06
2006 06
2006 06
2006 06
2006 06
2006 06
2006 06
2006 06
2006 06
2006 06
2006 06
2006 06
2006 06
2006 06
2006 06
2006 06
2006 06
2006 06
2006 06
2006 06
2006 06
2006 06
2006 06
2006 06
2006 06
[32047]
[32481]
[32489]
[32490]
[32491]
[32492]
[32493]
[32494]
[32495]
[32496]
[32497]
[32498]
[32499]
[34224]
[34225]
[34226]
[34227]
[34228]
[34229]
[34230]
[34231]
[34232]
[34233]
[34234]
[34235]
[34236]
[34237]
[34238]
[34239]
[34240]
[34241]
[34242]
AA
AB
AC
AD
AE
AF
AG
AH
AJ
AK
AL
AM
AN
AP
AQ
AR
AS
AT
AU
AV
AW
AX
AY
AZ
BA
BB
BC
BD
BE
BF
BG
BH
2014 - Version 1-13
(Compiled 2006)
Date of
orbital
Determination
Orbital
Inclination
(deg)
2007
2007
2007
2007
2007
2007
2007
2007
2007
2007
2007
2007
2007
2007
2007
2007
2008
2007
2008
2007
2008
2008
2008
2008
2008
2008
2008
2008
2008
2008
2008
2008
51.78
51.46
51.63
51.68
51.63
50.93
51.71
51.65
51.71
50.60
51.65
51.83
51.70
51.63
51.49
52.34
51.05
50.64
49.99
51.44
49.76
50.84
51.48
51.50
51.40
51.62
51.65
51.83
51.73
51.72
51.73
51.67
Aug
Aug
Aug
Aug
Aug
Aug
Aug
Aug
Aug
Aug
Aug
Jul
Aug
Aug
Aug
Aug
Jan
Aug
Mar
Aug
Feb
Feb
Feb
Feb
Feb
Feb
Feb
Feb
Feb
Feb
Feb
Feb
15.71
15.60
15.74
14.96
15.75
15.06
15.65
14.21
15.69
1.80
14.08
30.16
15.73
15.79
15.13
15.08
3.52
14.57
2.02
15.44
17.95
17.94
18.42
18.53
18.08
18.22
18.17
18.15
18.17
17.94
17.77
18.06
Nodal
period
(min)
Extra Page 2006 -2
Semi
major axis
(km)
273.70
279.30
264.48
276.17
275.62
273.78
275.45
247.38
275.82
301.37
273.55
266.58
274.98
277.77
301.67
291.35
98.82
271.08
94.80
264.67
271.13
264.77
225.25
263.12
273.27
272.13
275.42
252.85
277.42
274.57
275.97
273.23
13964
14154
13649
14048
14029
13967
14024
13749
14036
14890
13959
13721
14008
14102
14900
14559
7081
13875
6887
13655
13877
13659
12263
13602
13950
13911
14023
13246
14090
13994
14041
13948
Perigee
height
(km)
Apogee
height
(km)
Orbital
eccentric.
Argument
of perigee
(deg)
353
563
554
444
446
565
427
349
408
813
378
339
407
465
906
561
145
505
179
571
851
800
547
294
539
413
450
279
421
421
408
354
14818
14989
13987
14894
14856
14612
14863
14392
14907
16209
14783
14346
14851
14982
16137
15798
1260
14488
838
13981
14146
13760
11223
14153
14603
14651
14839
13455
15002
14810
14917
14786
0.518
0.510
0.492
0.514
0.514
0.503
0.515
0.511
0.517
0.517
0.516
0.510
0.516
0.515
0.511
0.523
0.079
0.504
0.048
0.491
0.479
0.474
0.435
0.509
0.504
0.512
0.513
0.497
0.517
0.514
0.517
0.517
294
292
297
293
293
299
293
297
293
286
294
288
294
293
283
286
336
303
123
299
52
62
103
48
36
38
34
50
31
34
33
37
RAE Table of Earth Satellites
Year of Launch 2006
Cospar ID
[Norad number]
D
2006
2006
2006
2006
2006
2006
2006
06
06
06
06
06
06
06
BJ
BK
BL
BM
BN
BP
BQ
[34243]
[34244]
[34245]
[34246]
[34247]
[34248]
[34249]
D
2006
2006
2006
2006
06
06
06
06
BR
BS
BT
BU
[34250]
[34251]
[34252]
[34253]
D
2006
2006
2006
2006
2006
2006
2006
2006
2006
2006
2006
2006
2006
2006
2006
2006
2006
2006
2006
2006
2006
2006
2006
2006
2006
2006
2006
2006
2006
2006
2006
06
06
06
06
06
06
06
06
06
06
06
06
06
06
06
06
06
06
06
06
06
06
06
06
06
06
06
06
06
06
06
BV
BW
BX
BY
BZ
CA
CB
CC
CD
CE
CF
CG
CH
CJ
CK
CL
CM
CN
CP
CQ
CR
CS
CT
CU
CV
CW
CX
CY
CZ
DA
DB
[34254]
[34255]
[34256]
[34257]
[34258]
[34259]
[34260]
[34261]
[34262]
[34263]
[35538]
[35539]
[35540]
[35541]
[35542]
[35543]
[35544]
[35545]
[35546]
[36958]
[36959]
[36960]
[36961]
[36962]
[36963]
[36964]
[38557]
[38558]
[38559]
[38560]
[38561]
2006
2006
2006
2006
2006
06
06
06
06
06
DC
DD
DE
DF
DG
[38562]
[38563]
[38564]
[39933]
[39934]
2014 - Version 1-13
Descent date
Lifetime
2014 Aug 20
3095 days
2013 Oct 14
2012 Sep 28
(Compiled 2006)
Date of
orbital
Determination
Orbital
Inclination
(deg)
2014 Aug 19.32
50.18
2013 Oct 14.73
51.64
2012
2012
2012
2012
2012
2012
2012
2012
2012
2013
2013
51.87
51.24
52.09
51.82
51.39
51.28
51.82
51.67
51.64
52.03
51.99
Nodal
period
(min)
Extra Page 2006 -3
Semi
major axis
(km)
Perigee
height
(km)
Apogee
height
(km)
Orbital
eccentric.
Argument
of perigee
(deg)
93.00 6800
269
572
0.022
157
90.30 6668
200
378
0.013
47
490
320
557
456
346
285
478
482
480
564
352
14044
10650
14971
14742
3273
1070
14599
14919
14721
15291
10013
0.497
0.435
0.510
0.511
0.179
0.056
0.507
0.513
0.509
0.514
0.418
212
47
93
129
224
54
160
142
169
171
211
2785 days
2404 days
Jul
Jun
Jul
Jun
Jul
Sep
Jul
Jun
Jul
Jam
Jun
7.33
27.48
6.71
10.65
7.06
25.13
7.50
13.66
2.64
12.22
23.84
264.38
214.33
278.97
274.08
122.90
98.30
272.32
277.08
274.13
283.82
206.18
13646
11864
14143
13977
8188
7056
13917
14079
13979
14306
11561
RAE Table of Earth Satellites
Year of Launch 2006
Cospar ID
[Norad number]
Descent date
Lifetime
Yaogan 1 CZ-4B 2nd stage fragments; 5 pieces, all in orbit
2006-15 C
[29536]
2006-15 D
[29537]
2006-15 E
[29538]
2006-15 F
[29539]
D 2006-15 G
[36363]
2012 Aug 4
2292 days
2006-15 H
2006-15 J
D
2006-22 F
[29235]
2006 Jul 6
19 days
D
2006-22 G
[29238]
2006 Jul 6
19 days
D
2006-22 H
[29239]
2006 Jul 7
20 days
Cosmos 2421 fragments, 329 pieces, 43 have decayed
2006-26 C
[32710]
2006-26 D
[32715]
2006-26 E
[32716]
D 2006-26 F
[32717]
2008 Apr 9
2006-26 G
[32718]
D
2006-26
2006-26
2006-26
2006-26
2006-26
2006-26
2006-26
2006-26
2006-26
2006-26
H
J
K
L
M
N
P
Q
R
S
[32719]
[32720]
[32721]
[32722]
[32723]
[32724]
[32725]
[32726]
[32727]
[32728]
D
2006-26 T
2006-26 U
D
2006-26
2006-26
2006-26
2006-26
2006-26
D
2006-26 AA
D
V
W
X
Y
Z
2014 - Version 1-13
Orbital
Inclination
(deg)
2006
2006
2006
2006
8.43
8.44
8.43
8.21
97.76
97.85
97.82
97.76
2012 Aug 4.83
2006
2006
2006
2006
2006
2006
2006
2006
Jun
Jul
Jun
Jul
Jun
Jul
Jun
Jul
2008
2008
2008
2008
2008
2008
2008
2008
2008
2008
2008
2008
2008
2008
2008
2008
2008
2008
2008
2008
2008
2008
2008
2008
2008
2008
2008
2008
Mar
Mar
Mar
Mar
Apr
Mar
Sep
Mar
Mar
Mar
Mar
Mar
Mar
Mar
Mar
Mar
Mar
Mar
Mar
Mar
Apr
Mar
Mar
Mar
Mar
Mar
Apr
Mar
Nov
Nov
Nov
Nov
Nodal
period
(min)
Extra Page 2006 -4
Semi
major axis
(km)
Perigee
height
(km)
Apogee
height
(km)
Orbital
eccentric.
Argument
of perigee
(deg)
7136
7139
7117
7113
619
619
612
616
895
902
864
853
0.019
0.020
0.018
0.017
307
309
293
295
97.87
88.07 6557
167
190
0.002
256
20.42
2.22
20.42
5.97
20.43
5.96
21.44
6.30
51.55
51.53
51.52
51.49
51.57
51.55
51.60
51.59
91.38
88.30
91.67
87.97
91.93
88.40
91.63
88.82
6721
6569
6735
6552
6748
6574
6733
6595
203
160
219
152
214
173
218
157
481
221
493
196
525
218
491
275
0.021
0.005
0.020
0.003
0.023
0.003
0.020
0.009
122
169
97
141
77
130
102
162
19.29
19.29
19.30
19.29
8.70
19.73
9.20
19.79
19.72
19.33
19.26
19.83
19.83
18.90
19.33
19.75
19.63
21.22
24.86
24.86
5.01
24.86
24.19
24.89
24.86
24.87
11.98
24.69
65.04
65.04
65.05
65.04
65.05
65.12
65.10
65.07
65.21
65.13
65.04
65.04
65.03
65.15
65.20
64.93
65.01
64.97
65.03
65.03
65.02
65.85
65.01
65.05
65.29
65.05
65.04
65.05
92.58
92.60
92.68
92.43
88.88
92.40
87.82
92.27
93.42
93.33
93.17
92.93
92.92
91.53
93.08
91.38
92.15
88.88
92.83
92.10
89.13
94.60
93.88
92.53
93.43
92.33
89.73
92.38
6780
6781
6784
6772
6598
6771
6545
6764
6820
6816
6808
6797
6796
6728
6804
6721
6758
6598
6792
6756
6611
6878
6843
6777
6821
6767
6639
6770
393
394
394
388
215
324
160
347
396
400
397
395
395
325
361
298
350
200
393
360
219
376
396
390
394
379
249
380
410
410
418
399
224
461
173
424
486
475
462
441
440
374
490
386
409
238
434
394
244
623
533
407
492
398
273
403
0.001
0.001
0.002
0.0008
0.0007
0.010
0.001
0.006
0.007
0.005
0.005
0.003
0.003
0.004
0.010
0.007
0.004
0.003
0.003
0.002
0.002
0.018
0.010
0.001
0.007
0.001
0.002
0.002
275
281
257
297
341
147
244
144
221
242
254
254
266
207
288
357
234
190
251
317
276
201
256
278
218
291
275
292
99.97
100.05
99.58
99.50
[36364]
[36365]
KazSat-1 Proton-K fragments; 4 pieces, all have decayed
D 2006-22 E
[29234]
2006 Jul 3
16 days
D
(Compiled 2006)
Date of
orbital
Determination
654 days
2008 Sep 9
2008 Mar 20
634 days
2008 Mar 21
635 days
[32732]
[32733]
2008 Apr 5
650 days
[32734]
[32735]
[32736]
[32737]
[32738]
2008 Apr 12
657 days
[32739]
2008 Apr 13
658 days
RAE Table of Earth Satellites
Year of Launch 2006
Cospar ID
[Norad number]
Descent date
Lifetime
(Compiled 2006)
Orbital
Inclination
(deg)
Perigee
height
(km)
Apogee
height
(km)
Orbital
eccentric.
Argument
of perigee
(deg)
2008
2008
2008
2008
2008
2008
2008
2008
2008
2008
2008
2008
2008
2008
2008
12.95
24.80
12.91
24.75
24.25
24.89
24.74
24.86
24.89
24.87
8.73
24.89
27.14
27.16
27.39
65.04
65.05
65.03
65.27
64.99
65.08
65.05
65.29
65.05
65.01
64.99
65.26
65.05
65.03
65.04
89.30
92.28
89.35
93.10
94.32
93.03
92.95
94.02
92.48
92.27
88.87
93.63
92.55
92.65
92.37
6619
6765
6621
6805
6864
6801
6798
6849
6774
6764
6597
6831
6778
6783
6769
227
384
231
398
398
372
392
394
385
381
200
393
389
388
379
253
390
253
454
573
474
447
548
407
390
237
512
409
421
402
0.002
0.0004
0.002
0.004
0.013
0.008
0.004
0.011
0.002
0.0006
0.003
0.009
0.001
0.002
0.002
257
271
278
252
251
283
252
264
235
260
266
221
284
239
276
2008 Apr 14.53
2008 Apr 13.56
65.03
65.04
89.28 6618
90.48 6676
227
286
252
309
0.002
0.002
276
272
2008 May 3.73
2008 May 8.76
65.04
65.05
90.08 6657
92.50 6776
265
382
292
412
0.002
0.002
314
264
65.05
65.00
65.15
65.08
65.05
65.11
65.05
65.07
65.05
65.10
65.00
65.31
63.81
65.76
65.11
65.04
65.08
65.16
65.07
92.73
92.45
96.22
92.83
89.50
92.70
92.57
92.62
89.25
92.65
92.47
94.20
91.60
97.93
92.93
92.25
92.68
92.73
92.18
6787
6773
6956
6792
6629
6785
6779
6781
6616
6783
6774
6858
6731
7039
6797
6763
6785
6787
6760
394
389
395
386
244
382
385
391
223
382
388
397
322
397
386
328
386
357
363
422
399
759
441
256
431
415
414
251
427
402
562
384
923
450
442
427
460
400
0.002
0.0008
0.026
0.004
0.0009
0.004
0.002
0.002
0.002
0.003
0.001
0.012
0.005
0.037
0.005
0.008
0.003
0.008
0.003
266
323
224
268
286
264
276
267
233
271
311
222
12
218
250
109
274
290
336
Apr
Mar
Apr
Mar
Mar
Mar
Mar
Mar
Mar
Mar
Apr
Mar
Mar
Mar
Mar
Nodal
period
(min)
Extra Page 2006 -5
Date of
orbital
Determination
Semi
major axis
(km)
D
2006-26 AB
[32740]
2008 Apr 13
658 days
D
2006-26
2006-26
2006-26
2006-26
2006-26
2006-26
2006-26
AC
AD
AE
AF
AG
AH
AJ
[32741]
[32742]
[32743]
[32744]
[32745]
[32746]
[32747]
2008 Apr 9
654 days
D
2006-26
2006-26
2006-26
2006-26
2006-26
2006-26
2006-26
2006-26
2006-26
2006-26
2006-26
2006-26
AK
AL
AM
AN
AP
AQ
AR
AS
AT
AU
AV
AW
[32748]
[32752]
[32753]
[32754]
[32758]
[32759]
[32760]
[32761]
[32762]
[32793]
[32796]
[32798]
D
2006-26
2006-26
2006-26
2006-26
AX
AY
AZ
BA
[32799]
[32800]
[32801]
[32802]
2008 Oct 28
856 days
D
2006-26 BB
2006-26 BC
2006-26 BD
[32803]
[32804]
[32805]
2008 Sep 6
804 days
D
2006-26
2006-26
2006-26
2006-26
2006-26
2006-26
2006-26
2006-26
2006-26
2006-26
BE
BF
BG
BH
BJ
BK
BL
BM
BN
BP
[32806]
[32807]
[32808]
[32809]
[32810]
[32811]
[32812]
[32813]
[32814]
[32815]
2008 Jun 19
725 days
2008
2008
2008
2008
2008
2008
2008
2008
2008
2008
2008
2008
2008
2008
2008
2008
2008
2008
2008
D
2006-26 BQ
[32816]
2008 Jun 19
725 days
2008 May 8.65
65.08
92.20 6761
365
399
0.002
338
D
2006-26
2006-26
2006-26
2006-26
2006-26
[32817]
[32818]
[32819]
[32820]
[32821]
2008
2008
2008
2008
2008
65.07
65.04
65.01
65.07
65.06
92.02
92.72
92.72
92.85
92.52
353
392
395
396
389
393
423
420
431
407
0.003
0.002
0.002
0.003
0.001
343
297
208
243
297
BR
BS
BT
BU
BV
2014 - Version 1-13
2008 Jun 20
2008 Sep 11
726 days
May
May
May
May
Oct
May
May
May
Sep
May
May
May
May
May
May
May
May
May
May
May
May
May
May
May
8.71
8.62
8.56
8.78
27.79
8.78
8.76
8.63
6.19
8.58
8.75
8.67
8.72
8.74
8.67
8.66
8.38
8.71
8.72
8.64
8.64
8.39
8.59
8.69
6752
6786
6786
6792
6777
RAE Table of Earth Satellites
Year of Launch 2006
Cospar ID
[Norad number]
Descent date
Lifetime
(Compiled 2006)
Nodal
period
(min)
Extra Page 2006 -6
Date of
orbital
Determination
Orbital
Inclination
(deg)
Semi
major axis
(km)
Sep
May
May
Sep
May
May
Sep
May
May
11.86
8.68
8.55
2.25
8.67
8.81
4.13
8.66
8.74
65.03
65.00
65.01
64.97
65.00
65.00
64.98
65.01
64.68
88.70
92.42
92.48
89.33
92.37
92.43
89.47
92.07
91.77
May
May
May
May
May
May
May
May
May
May
May
May
May
May
May
May
May
May
8.59
8.68
8.79
8.76
8.67
8.64
8.68
8.69
8.68
8.60
8.69
8.69
8.66
8.71
8.68
8.63
8.69
8.65
65.10
65.19
65.18
65.25
64.92
65.37
65.95
64.86
64.71
65.08
65.11
65.15
65.56
64.51
65.01
65.07
65.11
65.05
92.82
92.52
93.45
93.78
94.17
94.52
98.02
91.85
91.02
92.20
93.10
93.05
93.45
92.17
92.52
92.67
91.82
92.15
Perigee
height
(km)
Apogee
height
(km)
Orbital
eccentric.
Argument
of perigee
(deg)
6589
6771
6774
6620
6769
6772
6626
6755
6740
198
387
391
229
384
388
236
367
324
221
398
400
254
396
399
259
386
399
0.002
0.0009
0.0007
0.002
0.0009
0.0008
0.002
0.001
0.006
243
331
328
229
335
338
239
335
336
6791
6776
6822
6838
6857
6874
7042
6744
6703
6761
6805
6803
6822
6759
6777
6783
6743
6758
389
369
380
373
379
399
400
330
271
368
388
388
389
363
394
393
341
365
436
426
507
546
578
592
928
401
378
397
465
460
496
398
402
417
386
394
0.003
0.004
0.009
0.013
0.014
0.014
0.037
0.005
0.008
0.002
0.006
0.005
0.008
0.003
0.0006
0.002
0.003
0.002
264
304
258
254
175
222
211
332
75
324
247
242
241
37
318
276
353
330
D
2006-26 BW
2006-26 BX
[32822]
[32823]
2008 Sep 2
800 days
D
2006-26 BY
2006-26 BZ
[32824]
[32825]
2008 Sep 4
802 days
D
2006-26 CA
2006-26 CB
[32826]
[32827]
2008 Jun 20
726 days
2008
2008
2008
2008
2008
2008
2008
2008
2008
D
2006-26
2006-26
2006-26
2006-26
2006-26
2006-26
2006-26
2006-26
2006-26
2006-26
2006-26
2006-26
2006-26
2006-26
2006-26
2006-26
2006-26
2006-26
CC
CD
CE
CF
CG
CH
CJ
CK
CL
CM
CN
CP
CQ
CR
CS
CT
CU
CV
[32828]
[32829]
[32830]
[32831]
[32832]
[32833]
[32834]
[32835]
[32836]
[32837]
[32838]
[32839]
[32840]
[32841]
[32842]
[32843]
[32844]
[32845]
725 days
2008
2008
2008
2008
2008
2008
2008
2008
2008
2008
2008
2008
2008
2008
2008
2008
2008
2008
D
2006-26 CW
2006-26 CX
2006-26 CY
[32846]
[32795]
[32849]
2008 Jun 27
733 days
2008 May 8.66
2008 May 14.50
2008 May 14.49
64.94
65.10
65.09
92.35 6768
92.60 6780
92.55 6778
370
380
378
408
423
420
0.003
0.003
0.003
332
269
272
D
2006-26 CZ
2006-26 DA
[32850]
[32851]
2008 Jun 26
732 days
2008 May 14.48
2008 May 14.31
65.13
65.08
92.83 6792
92.23 6763
380
371
446
398
0.005
0.002
258
318
D
2006-26
2006-26
2006-26
2006-26
2006-26
2006-26
2006-26
2006-26
2006-26
2006-26
DB
DC
DD
DE
DF
DG
DH
DJ
DK
DL
[32852]
[32853]
[32854]
[32855]
[32856]
[32857]
[32858]
[32859]
[32860]
[32861]
2008 Jun 22
728 days
D
2006-26
2006-26
2006-26
2006-26
DM
DN
DP
DQ
[32862]
[32863]
[32864]
[32865]
2008 Jun 27
733 days
2008
2008
2008
2008
2008
2008
2008
2008
2008
2008
2008
2008
2008
2008
2008
65.16
65.07
65.07
65.06
65.13
65.05
65.07
65.11
65.04
65.05
65.02
65.05
65.07
65.08
65.13
92.82
92.20
92.10
91.83
92.90
92.25
92.72
92.52
92.32
92.33
88.92
92.48
92.27
92.22
92.65
384
357
361
345
389
372
363
376
374
375
204
383
370
368
378
441
391
395
385
445
399
451
420
402
403
238
409
401
399
430
0.004
0.003
0.003
0.003
0.004
0.002
0.006
0.003
0.002
0.002
0.003
0.002
0.002
0.002
0.004
257
328
334
337
258
312
318
275
292
291
250
289
285
298
263
2014 - Version 1-13
2008 Jun 19
May
May
May
May
May
May
May
May
May
May
Sep
May
May
May
May
14.53
14.54
14.68
14.58
14.67
14.31
14.56
14.68
14.71
14.52
22.82
14.60
14.72
14.71
14.51
6791
6752
6756
6743
6795
6764
6786
6777
6766
6768
6600
6775
6764
6762
6783
RAE Table of Earth Satellites
Year of Launch 2006
Cospar ID
[Norad number]
Descent date
Lifetime
(Compiled 2006)
Date of
orbital
Determination
Orbital
Inclination
(deg)
2008 May 14.66
2008 Sep 27.28
2008 May 14.52
65.00
65.00
65.04
May
Oct
May
Nov
May
May
May
May
May
May
May
Oct
May
May
May
May
May
May
May
May
Oct
May
May
May
14.67
1.98
14.55
3.01
14.53
14.56
14.53
14.68
14.56
14.68
14.54
2.59
14.57
14.80
14.47
14.53
14.64
14.70
14.65
14.72
2.04
14.69
14.67
14.69
May
May
May
May
May
Nodal
period
(min)
Extra Page 2006 -7
Semi
major axis
(km)
Perigee
height
(km)
Apogee
height
(km)
Orbital
eccentric.
Argument
of perigee
(deg)
92.88 6794
88.78 6593
92.33 6767
391
203
375
440
225
402
0.004
0.002
0.002
258
279
294
65.01
64.99
65.05
65.02
65.01
64.32
64.15
65.09
65.06
65.04
65.03
65.01
65.08
65.08
65.03
65.11
65.09
64.79
65.08
64.96
64.93
65.12
65.13
65.06
92.52
88.48
92.60
89.45
92.43
91.52
91.60
91.80
91.67
92.62
92.88
88.97
93.02
91.57
91.58
92.83
91.83
91.52
91.83
92.12
89.05
92.60
92.90
92.28
6776
6578
6781
6626
6772
6728
6732
6741
6735
6781
6795
6602
6801
6730
6731
6792
6743
6728
6743
6757
6606
6781
6795
6765
393
189
376
240
390
302
326
337
335
390
391
214
381
330
336
389
344
339
346
360
214
380
389
373
402
210
429
254
398
397
379
388
377
416
441
232
464
372
368
438
385
358
383
396
241
424
445
400
0.0006
0.002
0.004
0.001
0.0006
0.007
0.004
0.004
0.003
0.002
0.004
0.001
0.006
0.003
0.002
0.004
0.003
0.001
0.003
0.003
0.002
0.003
0.004
0.002
271
299
288
250
300
4
55
351
341
287
253
330
256
351
308
260
336
45
331
26
301
269
258
327
14.55
14.55
14.67
14.64
14.73
65.05
65.05
65.04
65.10
65.09
92.60
92.62
92.57
92.68
92.05
6780
6781
6779
6785
6753
390
390
387
382
357
414
415
413
430
392
0.002
0.002
0.002
0.004
0.003
287
289
284
261
334
D
2006-26 DR
[32866]
2008 Sep 27
824 days
D
2006-26 DS
[32867]
2008 Jun 27
733 days
D
2006-26 DT
[32868]
2008 Oct 2
829 days
D
2006-26 DU
[32869]
2008 Nov 3
861 days
D
2006-26
2006-26
2006-26
2006-26
2006-26
2006-26
2006-26
DV
DW
DX
DY
DZ
EA
EB
[32870]
[32871]
[32872]
[32873]
[32874]
[32875]
[32876]
2008 Oct 2
829 days
D
2006-26
2006-26
2006-26
2006-26
2006-26
2006-26
2006-26
2006-26
EC
ED
EE
EF
EG
EH
EJ
EK
[32877]
[32878]
[32879]
[32880]
[32881]
[32882]
[32883]
[32884]
2008 Oct 2
829 days
D
2006-26 EL
2006-26 EM
2006-26 EN
[32885]
[32886]
[32887]
2008 Jun 23
729 days
2008
2008
2008
2008
2008
2008
2008
2008
2008
2008
2008
2008
2008
2008
2008
2008
2008
2008
2008
2008
2008
2008
2008
2008
D
2006-26
2006-26
2006-26
2006-26
2006-26
EP
EQ
ER
ES
ET
[32888]
[32889]
[32890]
[32891]
[32892]
2008 Jun 25
731 days
2008
2008
2008
2008
2008
D
2006-26 EU
[32893]
2008 Jun 21
727 days
2008 May 14.73
65.07
92.12 6757
362
395
0.002
339
D
2006-26 EV
[32894]
2008 Jun 21
727 days
2008 May 14.61
65.07
92.07 6754
358
393
0.003
327
D
2006-26 EW
[32895]
2008 Jun 19
725 days
2008 May 14.55
65.08
92.17 6759
363
398
0.003
323
D
2006-26 EX
[32896]
2008 Oct 2
829 days
D
2006-26
2006-26
2006-26
2006-26
2006-26
EY
EZ
FA
FB
FC
[32897]
[32898]
[32899]
[32900]
[32901]
2008 Oct 23
850 days
2006-26 FD
[32902]
2008
2008
2008
2008
2008
2008
2008
2008
2008
65.00
64.98
65.11
65.07
65.09
64.98
65.04
65.04
65.12
92.40
88.28
92.63
92.67
92.57
92.30
92.45
89.87
92.87
385
180
378
380
376
378
379
259
389
398
200
428
430
425
397
410
277
441
0.001
0.002
0.004
0.004
0.004
0.001
0.002
0.001
0.004
342
291
266
263
271
255
312
308
255
2014 - Version 1-13
May
Oct
May
May
May
May
May
Oct
May
14.65
1.92
14.57
14.58
14.69
14.67
14.59
22.29
14.73
6770
6568
6782
6784
6779
6766
6773
6646
6794
RAE Table of Earth Satellites
Year of Launch 2006
Cospar ID
[Norad number]
Descent date
Lifetime
D
2006-26
2006-26
2006-26
2006-26
2006-26
2006-26
2006-26
2006-26
2006-26
FE
FF
FG
FH
FJ
FK
FL
FM
FN
[32903]
[32904]
[32905]
[32906]
[32907]
[32908]
[32909]
[32910]
[32911]
2008 Jun 23
729 days
D
2006-26 FP
[32912]
2008 Nov 9
867 days
D
2006-26
2006-26
2006-26
2006-26
2006-26
2006-26
2006-26
FQ
FR
FS
FT
FU
FV
FW
[32913]
[32914]
[32915]
[32916]
[32917]
[32918]
[32919]
2008 Sep 18
815 days
D
2006-26 FX
2006-26 FY
[32920]
[32921]
2008 Jun 23
729 days
D
2006-26 FZ
2006-26 GA
2006-26 GB
[32922]
[32923]
[32924]
2008 Nov 8
866 days
D
2006-26 GC
[32925]
2008 Nov 5
863 days
D
2006-26 GD
2006-26 GE
[32926]
[32927]
2008 Jun 19
725 days
D
2006-26 GF
[32928]
2008 Nov 1
859 days
D
2006-26 GG
[32929]
2008 Sep 11
808 days
D
2006-26 GH
2006-26 GJ
[32930]
[32931]
2008 Jun 21
727 days
D
2006-26 GK
2006-26 GL
[32932]
[32933]
2008 Sep 25
822 days
2006-26
2006-26
2006-26
2006-26
2006-26
2006-26
2006-26
2006-26
2006-26
[32934]
[32935]
[32936]
[32937]
[32938]
[32939]
[32940]
[32941]
[32942]
GM
GN
GP
GQ
GR
GS
GT
GU
GV
2014 - Version 1-13
(Compiled 2006)
Nodal
period
(min)
Extra Page 2006 -8
Date of
orbital
Determination
Orbital
Inclination
(deg)
Semi
major axis
(km)
Perigee
height
(km)
Apogee
height
(km)
Orbital
eccentric.
Argument
of perigee
(deg)
2008
2008
2008
2008
2008
2008
2008
2008
2008
May
May
May
May
May
May
May
May
May
14.74
20.16
20.43
20.54
20.55
20.30
20.53
20.53
20.56
64.93
65.05
65.04
65.00
65.08
65.09
65.12
65.03
65.08
91.38
92.17
92.28
92.53
91.85
91.65
92.85
92.58
92.02
6721
6759
6765
6777
6744
6734
6792
6780
6752
331
369
373
390
348
336
389
394
358
353
392
400
408
382
375
438
409
389
0.002
0.002
0.002
0.001
0.003
0.003
0.004
0.001
0.002
28
288
290
184
324
341
258
283
325
2008
2008
2008
2008
2008
2008
2008
2008
2008
2008
2008
2008
May
Nov
May
May
May
May
May
May
May
Sep
May
May
20.53
8.41
20.56
20.22
20.24
20.56
20.49
20.57
20.56
15.11
20.53
20.55
65.10
65.11
65.22
63.66
65.05
65.08
65.02
65.00
65.00
64.98
65.07
65.04
92.83
89.73
93.15
93.18
92.22
91.23
91.75
91.87
92.38
89.57
91.75
92.20
6792
6640
6807
6809
6762
6713
6739
6745
6770
6632
6739
6761
389
256
385
386
368
313
349
357
385
240
344
370
437
266
473
475
398
356
372
375
397
266
377
395
0.004
0.0008
0.007
0.007
0.002
0.003
0.002
0.001
0.0009
0.002
0.002
0.002
259
129
241
262
284
337
315
319
321
249
328
284
2008
2008
2008
2008
2008
2008
2008
2008
May
May
May
Nov
May
Nov
May
May
20.07
20.43
20.59
8.37
20.53
3.08
20.54
20.52
65.17
65.11
65.11
65.08
65.13
65.10
65.12
65.09
92.62
92.25
92.80
89.02
92.83
89.53
92.92
92.13
6782
6763
6791
6604
6792
6630
6796
6758
366
365
387
218
388
244
392
368
440
405
437
232
439
259
443
390
0.005
0.003
0.004
0.001
0.004
0.001
0.004
0.002
265
286
258
192
257
353
252
321
2008
2008
2008
2008
2008
2008
May
Nov
May
Sep
May
May
20.57
1.94
20.57
10.08
20.56
20.38
65.10
65.09
65.01
64.98
65.01
65.06
92.75
89.98
92.43
88.83
91.97
92.10
6788
6603
6773
6596
6749
6756
387
219
388
205
364
364
431
230
399
229
378
392
0.003
0.0009
0.0008
0.002
0.001
0.002
263
302
296
253
23
317
2008
2008
2008
2008
2008
2008
2008
2008
2008
2008
2008
2008
May
May
Sep
May
May
May
May
May
May
May
May
May
20.53
20.62
24.64
20.54
20.36
20.53
20.52
20.57
20.39
20.36
20.23
20.58
65.05
65.00
64.97
65.10
65.08
65.08
65.11
65.12
65.05
65.05
65.05
65.04
92.20
92.40
88.57
92.45
92.50
92.83
92.82
92.65
92.02
92.25
92.23
92.48
6761
6771
6582
6773
6775
6792
6791
6783
6752
6764
6762
6775
369
386
192
373
372
388
388
374
360
372
371
384
395
399
214
416
421
438
436
435
386
399
396
408
0.002
0.0009
0.002
0.003
0.004
0.004
0.004
0.004
0.002
0.002
0.002
0.002
309
330
282
268
264
259
259
267
299
298
296
287
RAE Table of Earth Satellites
Year of Launch 2006
Cospar ID
[Norad number]
Descent date
Lifetime
D
2006-26
2006-26
2006-26
2006-26
GW
GX
GY
GZ
[32943]
[32944]
[32945]
[32946]
D
2006-26
2006-26
2006-26
2006-26
2006-26
2006-26
2006-26
2006-26
2006-26
HA
HB
HC
HD
HE
HF
HG
HH
HJ
[32947]
[32948]
[32949]
[32950]
[33001]
[33002]
[33003]
[33004]
[33005]
D
2006-26 HK
2006-26 HL
2006-26 HM
[33006]
[33007]
[33008]
2008 Jun 22
728 days
D
2006-26 HN
[33009]
2008 Aug 27
794 days
D
2006-26 HP
2006-26 HQ
[33010]
[33011]
D
2006-26
2006-26
2006-26
2006-26
2006-26
HR
HS
HT
HU
HV
[33012]
[33013]
[33014]
[33015]
[33016]
2008 Jun 6
712 days
D
2006-26 HW
[33017]
2008 Sep 7
805 days
D
2006-26 HX
[33018]
2008 Jun 19
725 days
D
2006-26
2006-26
2006-26
2006-26
HY
HZ
JA
JB
[33019]
[33020]
[33021]
[33022]
2008 Jun 26
732 days
D
2006-26 JC
[33023]
2008 Oct 25
852 days
D
2006-26 JD
2006-26 JE
[33024]
[33025]
D
2006-26 JF
2006-26 JG
[33026]
[33027]
2006-26
2006-26
2006-26
2006-26
[33028]
[33029]
[33030]
[33031]
JH
JJ
JK
JL
2014 - Version 1-13
2008 Jun 27
2008 Oct 28
2008 Oct 23
733 days
(Compiled 2006)
Nodal
period
(min)
Extra Page 2006 -9
Date of
orbital
Determination
Orbital
Inclination
(deg)
Semi
major axis
(km)
Perigee
height
(km)
Apogee
height
(km)
Orbital
eccentric.
Argument
of perigee
(deg)
2008
2008
2008
2008
May
May
May
May
20.55
20.39
20.54
20.41
65.09
65.11
64.99
65.05
92.50
92.75
91.72
92.15
6775
6788
6737
6759
373
386
349
367
420
432
367
392
0.004
0.003
0.001
0.002
266
257
332
306
2008
2008
2008
2008
May
May
May
May
20.38
20.58
20.23
20.56
65.03
65.07
65.05
65.11
91.75
91.87
91.78
92.55
6739
6744
6740
6778
347
353
351
376
374
379
373
423
0.002
0.002
0.002
0.003
296
287
337
267
2008 Oct 27.71
65.08
89.33 6620
236
247
0.0009
274
2008 Aug 27.03
65.04
88.85 6597
206
229
0.002
237
2008 Oct 23.31
65.00
89.32 6619
232
249
0.001
306
2008 Sep
4.18
64.99
89.77 6641
251
274
0.002
233
2008 Oct 23.66
65.06
89.87 6646
258
277
0.004
328
855 days
850 days
2008 Jun 13
719 days
2008 Jun 24
730 days
RAE Table of Earth Satellites
Year of Launch 2006
Cospar ID
[Norad number]
Descent date
Lifetime
D
2006-26
2006-26
2006-26
2006-26
2006-26
2006-26
2006-26
2006-26
JM
JN
JP
JQ
JR
JS
JT
JU
[33032]
[33033]
[33034]
[33035]
[33036]
[33037]
[33038]
[33039]
2008 Jun 13
719 days
D
2006-26
2006-26
2006-26
2006-26
2006-26
2006-26
2006-26
JV
JW
JX
JY
JZ
KA
KB
[33040]
[33041]
[33042]
[33043]
[33044]
[33045]
[33046]
2008 Sep 7
805 days
D
2006-26 KC
[33047]
2008 Oct 20
848 days
D
2006-26 KD
[33048]
2008 Oct 15
843 days
D
2006-26 KE
2006-26 KF
[33049]
[33050]
2008 Jun 19
725 days
D
2006-26 KG
[33068]
2008 Jun 24
730 days
D
2006-26 KH
[33069]
2008 Jun 24
730 days
D
2006-26 KJ
2006-26 KK
2006-26 KL
[33070]
[33071]
[33072]
2008 Oct 3
830 days
D
2006-26
2006-26
2006-26
2006-26
2006-26
2006-26
2006-26
2006-26
2006-26
KM
KN
KP
KQ
KR
KS
KT
KU
KV
[33073]
[33074]
[33075]
[33076]
[33077]
[33078]
[33079]
[33080]
[33081]
D
2006-26 KW
2006-26 KX
2006-26 KY
[33082]
[33083]
[33084]
D
2006-26
2006-26
2006-26
2006-26
[33085]
[33086]
[33087]
[33088]
Date of
orbital
Determination
2008 Sep
KZ
LA
LB
LC
2014 - Version 1-13
2008 Sep 10
2008 Sep 3
(Compiled 2006)
Orbital
Inclination
(deg)
Nodal
period
(min)
Extra Page 2006 -10
Semi
major axis
(km)
Perigee
height
(km)
Apogee
height
(km)
Orbital
eccentric.
Argument
of perigee
(deg)
3.89
65.00
89.78 6642
255
272
0.001
233
2008 Oct 19.63
65.06
88.55 6581
195
210
0.001
326
2008 Oct 14.42
65.07
89.67 6636
244
271
0.002
304
2008 Oct 1.78
64.98
89.82 6644
251
279
0.002
269
2008 Aug 20.05
64.95
91.40 6722
323
364
0.003
196
2008 Aug 31.98
65.01
89.60 6633
247
263
0.001
235
2008 Aug 27.03
64.99
88.57 6582
194
213
0.001
247
808 days
801 days
RAE Table of Earth Satellites
Year of Launch 2006
Cospar ID
[Norad number]
Descent date
Lifetime
2008 Nov 2
861 days
D
2006-26 LD
2006-26 LE
2006-26 LF
[33089]
[33090]
[33091]
D
2006-26 LG
2006-26 LH
[33092]
[33093]
2008 Jun 27
733 days
D
2006-26 LJ
2006-26 LK
2006-26 LL
[33094]
[33095]
[33096]
2008 Jun 21
727 days
D
2006-26 LM
[33097]
2008 Nov 5
864 days
D
2006-26 LN
2006-26 LP
2006-26 LQ
[33098]
[33099]
[33100]
2008 Jun 27
733 days
D
2006-26 LR
[33101]
2008 Sep 25
823 days
D
2006-26 LS
2006-26 LT
2006-26 LU
[33102]
[33103]
[33104]
2008 Jun 24
730 days
D
2006-26 LV
2006-26 LW
2006-26 LX
[33107]
[33114]
[33115]
2008 Sep 3
801 days
D
2006-26 LY
2006-26 LZ
[33116]
[33117]
D
2006-26
2006-26
2006-26
2006-26
MA
MB
MC
MD
[33118]
[33119]
[33120]
[33121]
2008 Sep 23
821 days
D
2006-26 ME
[33122]
2008 Oct 5
833 days
D
2006-26 MF
2006-26 MG
[33123]
[33124]
D
2006-26 MH
2006-26 MJ
[33125]
[33126]
D
2006-26
2006-26
2006-26
2006-26
2006-26
2006-26
2006-26
2006-26
[33127]
[33128]
[33129]
[33130]
[33131]
[33132]
[33133]
[33134]
MK
ML
MM
MN
MP
MQ
MR
MS
2014 - Version 1-13
2008 Sep 27
2008 Aug 29
2008 Oct 18
2008 Nov 2
(Compiled 2006)
Date of
orbital
Determination
Orbital
Inclination
(deg)
2008 Nov 1.48
64.81
2008 Nov 5.14
Nodal
period
(min)
Extra Page 2006 -11
Semi
major axis
(km)
Perigee
height
(km)
Apogee
height
(km)
Orbital
eccentric.
Argument
of perigee
(deg)
89.93 6649
268
273
0.0003
108
64.99
89.40 6623
242
248
0.0004
281
2008 Sep 24.87
64.97
89.52 6629
236
265
0.002
255
2008 Sep 1.22
64.97
89.35 6621
228
256
0.002
220
2008 Sep 26.96
65.05
88.70 6589
197
222
0.002
290
2008 Sep 23.25
65.02
88.65 6586
196
219
0.002
268
2008 Oct 5.54
65.02
89.22 6615
227
244
0.001
275
2008 Aug 29.40
65.01
89.50 6628
238
261
0.002
218
2008 Oct 17.34
65.02
89.87 6646
257
278
0.002
307
825 days
796 days
846 days
861 days
RAE Table of Earth Satellites
Year of Launch 2006
Cospar ID
[Norad number]
Descent date
Lifetime
D
2006-26 MT
[33135]
2008 Sep 12
810 days
D
2006-26 MU
[33136]
2008 Oct 20
848 days
D
2006-26 MV
2006-26 MW
[33137]
[33138]
D
2006-26
2006-26
2006-26
2006-26
2006-26
2006-26
MX
MY
MZ
NA
NB
NC
[33139]
[33140]
[33141]
[33142]
[33143]
[33144]
2008 Nov 1
860 days
D
2006-26 ND
[33145]
2008 Oct 28
856 days
D
2006-26 NE
[33146]
2008 Aug 28
795 days
D
2006-26 NF
2006-26 NG
[33147]
[33148]
2008 Oct 18
846 days
D
2006-26 NH
[33149]
2008 Oct 20
848 days
D
2006-26 NJ
2006-26 NK
[33150]
[33151]
D
2006-26
2006-26
2006-26
2006-26
2006-26
NL
NM
NN
NP
NQ
[33152]
[33157]
[33158]
[33159]
[33160]
D
2006-26
2006-26
2006-26
2006-26
NR
NS
NT
NU
[33161]
[33162]
[33163]
[33164]
D
2006-26 NV
2006-26 NW
2006-26 NX
[33165]
[33166]
[33167]
D
2006-26 NY
2006-26 NZ
[33168]
[33169]
D
2006-26 PA
2006-26 PB
2006-26 PC
[33170]
[33171]
[33172]
2008 Sep 23
821 days
D
2006-26 PD
[33173]
2008 Sep 4
802 days
2014 - Version 1-13
2008 Oct 4
2008 Sep 23
2008 Oct 26
2008 Nov 7
2008 Nov 1
2008 Oct 15
(Compiled 2006)
Date of
orbital
Determination
Orbital
Inclination
(deg)
2008 Nov 1.92
65.00
2008 Sep 12.17
Nodal
period
(min)
Extra Page 2006 -12
Semi
major axis
(km)
Perigee
height
(km)
Apogee
height
(km)
Orbital
eccentric.
Argument
of perigee
(deg)
89.35 6621
239
246
0.0005
288
65.04
88.58 6583
183
225
0.003
229
2008 Oct 20.24
65.85
89.05 6606
225
230
0.0004
333
2008 Oct 4.84
65.02
89.12 6610
218
244
0.002
297
2008 Nov 1.48
65.02
89.43 6625
240
253
0.001
300
2008 Oct 27.60
65.02
88.37 6572
189
198
0.0007
343
2008 Aug 28
64.99
89.23 6615
224
249
0.002
215
2008 Oct 18.22
65.02
89.02 6605
215
237
0.002
305
2008 Oct 20.32
65.02
89.43 6625
238
255
0.001
326
2008 Sep 22.68
64.96
88.47 6577
192
205
0.0009
264
2008 Oct 26.67
65.00
88.90 6598
214
226
0.0009
353
2008 Nov 7.47
65.01
89.18 6612
231
237
0.0004
203
2008 Nov 1.45
65.01
89.43 6625
244
249
0.0004
333
2008 Oct 15.45
64.95
88.38 6573
184
206
0.002
317
2008 Sep 23.55
64.99
88.17 6562
174
194
0.002
222
2008 Sep
64.96
89.67 6636
248
268
0.002
235
832 days
821 days
854 days
867 days
860 days
843 days
3.17
RAE Table of Earth Satellites
Year of Launch 2006
Cospar ID
[Norad number]
Descent date
Lifetime
D
2006-26 PE
[33174]
2008 Oct 3
831 days
D
2006-26 PF
[33175]
2008 Oct 22
850 days
D
2006-26
2006-26
2006-26
2006-26
2006-26
PG
PH
PJ
PK
PL
[33176]
[33177]
[33178]
[33179]
[33180]
2008 Oct 10
838 days
D
2006-26 PM
[33181]
2008 Oct 19
847 days
D
2006-26 PN
[33182]
2008 Oct 2
830 days
D
2006-26 PP
[33183]
2008 Aug 28
795 days
D
2006-26
2006-26
2006-26
2006-26
2006-26
2006-26
2006-26
2006-26
2006-26
2006-26
2006-26
2006-26
2006-26
2006-26
2006-26
2006-26
PQ
PR
PS
PT
PU
PV
PW
PX
PY
PZ
QA
QB
QC
QD
QE
QF
[33184]
[33185]
[33186]
[33187]
[33188]
[33189]
[33190]
[33191]
[33192]
[33193]
[33194]
[33195]
[33196]
[33197]
[33198]
[33199]
D
2006-26 QG
2006-26 QH
[33200]
[33201]
2008 Oct 19
847 days
D
2006-26 QJ
[33209]
2008 Sep 28
826 days
D
2006-26 QK
2006-26 QL
[33210]
[33211]
D
2006-26 QM
2006-26 QN
[33212]
[33213]
D
2006-26 QP
2006-26 QQ
2006-26 QR
[33214]
[33215]
[33216]
D
2006-26 QS
2006-26 QT
[33217]
[33218]
2014 - Version 1-13
2008 Sep 12
2008 Sep 2
2008 Oct 21
2008 Oct 5
(Compiled 2006)
Date of
orbital
Determination
Orbital
Inclination
(deg)
2008 Oct 3.51
64.99
2008 Oct 22.62
Nodal
period
(min)
Extra Page 2006 -13
Semi
major axis
(km)
Perigee
height
(km)
Apogee
height
(km)
Orbital
eccentric.
Argument
of perigee
(deg)
88.95 6602
217
228
0.0008
297
64.75
89.17 6612
227
239
0.0009
319
2008 Oct 9.71
65.04
88.65 6587
200
216
0.001
190
2008 Oct 19.62
65.02
89.02 6605
215
237
0.002
332
2008 Oct 2.48
65.00
88.85 6596
206
229
0.002
306
2008 Aug 28.00
64.97
88.28 6568
179
200
0.002
241
2008 Aug 4.54
65.00
91.43 6723
330
359
0.002
276
2008 Oct 18.03
65.01
89.35 6621
217
268
0.004
348
2008 Sep 28.16
65.01
89.27 6617
226
250
0.002
274
2008 Sep 2.17
65.02
88.70 6589
190
230
0.003
202
2008 Oct 21.34
65.02
89.42 6624
236
255
0.001
337
2008 Oct 4.45
65.06
88.82 6595
201
231
0.002
303
2008 Oct 20.35
65.01
88.98 6603
214
234
0.002
325
810 days
800 days
849 days
833 days
RAE Table of Earth Satellites
Year of Launch 2006
Cospar ID
[Norad number]
Descent date
Lifetime
D
2006-26
2006-26
2006-26
2006-26
2006-26
2006-26
QU
QV
QW
QX
QY
QZ
[33219]
[33220]
[33221]
[33222]
[33223]
[33224]
2008 Oct 22
850 days
D
2006-26 RA
[33225]
2008 Sep 3
801 days
D
2006-26
2006-26
2006-26
2006-26
2006-26
2006-26
2006-26
2006-26
RB
RC
RD
RE
RF
RG
RH
RJ
[33226]
[33227]
[33228]
[33229]
[33230]
[33231]
[33232]
[33233]
D
2006-26 RK
2006-26 RL
[33234]
[33235]
D
2006-26
2006-26
2006-26
2006-26
RM
RN
RP
RQ
[33236]
[33237]
[33238]
[33239]
2008 Sep 12
810 days
D
2006-26 RR
[33240]
2008 Aug 27
794 days
D
2006-26 RS
2006-26 RT
2006-26 RU
[33241]
[33242]
[33246]
D
2006-26
2006-26
2006-26
2006-26
RV
RW
RX
RY
[33247]
[33248]
[33249]
[33250]
D
2006-26
2006-26
2006-26
2006-26
2006-26
RZ
SA
SB
SC
SD
[33251]
[33252]
[33253]
[33254]
[33255]
D
2006-26 SE
2006-26 SF
[33256]
[33257]
2008 Oct 10
838 days
D
2006-26 SG
[33258]
2008 Oct 5
833 days
D
2006-26 SH
[33259]
2008 Aug 27
794 days
2006-26 SJ
[33260]
2014 - Version 1-13
2008 Sep 16
2008 Sep 16
2008 Oct 10
2008 Oct 10
2008 Oct 5
(Compiled 2006)
Date of
orbital
Determination
Orbital
Inclination
(deg)
2008 Oct 22.27
65.01
2008 Sep 1.21
Nodal
period
(min)
Extra Page 2006 -14
Semi
major axis
(km)
Perigee
height
(km)
Apogee
height
(km)
Orbital
eccentric.
Argument
of perigee
(deg)
88.68 6588
205
215
0.0007
327
65.08
89.12 6609
218
243
0.002
234
2008 Sep 16.15
65.03
89.18 6613
220
249
0.002
235
2008 Sep 16.06
65.04
89.53 6630
242
260
0.001
253
2008 Sep 12.08
65.08
89.17 6612
217
250
0.003
242
2008 Aug 26.85
64.97
88.30 6569
163
218
0.004
185
2008 Oct 10.77
65.05
89.07 6607
214
242
0.002
337
2008 Oct 9.75
64.98
88.88 6598
207
231
0.002
312
2008 Oct 5.18
64.99
88.82 6595
205
227
0.002
308
2008 Oct 10.33
65.02
89.33 6620
229
254
0.002
321
2008 Oct 3.50
64.99
90.32 6669
280
301
0.002
274
2008 Aug 27.31
64.86
89.88 6647
251
286
0.003
193
814 days
814 days
838 days
838 days
833 days
RAE Table of Earth Satellites
Year of Launch 2006
Cospar ID
[Norad number]
Descent date
Lifetime
2008 Aug 29
796 days
D
2006-26 SK
2006-26 SL
[33261]
[33262]
D
2006-26 SM
2006-26 SN
2006-26 SP
[33263]
[33264]
[33265]
D
2006-26
2006-26
2006-26
2006-26
2006-26
SQ
SR
SS
ST
SU
[33266]
[33267]
[33268]
[33269]
[33270]
D
2006-26 SV
2006-26 SW
[33271]
[33282]
D
2006-26 SX
2006-26 SY
[33283]
[33284]
2008 Aug 28
795 days
D
2006-26 SZ
[33285]
2008 Aug 28
795 days
D
2006-26 TA
[33286]
2008 Nov 4
863 days
D
2006-26 TB
2006-26 TC
2006-26 TD
[33287]
[33288]
[33289]
2008 Oct 20
848 days
D
2006-26 TE
[33290]
2008 Oct 21
849 days
D
2006-26 TF
[33291]
2008 Sep 26
824 days
D
2006-26 TG
[33292]
2008 Oct 29
857 days
D
2006-26 TH
[33293]
2008 Sep 10
808 days
D
2006-26 TJ
[33294]
2008 Sep 22
820 days
D
2006-26 TK
2006-26 TL
2006-26 TM
[33295]
[33296]
[33297]
D
2006-26 TN
2006-26 TP
2006-26 TQ
[33298]
[33299]
[33300]
2008 Aug 30
797 days
D
2006-26 TR
[33301]
2008 Sep 26
824 days
D
2006-26
2006-26
2006-26
2006-26
[33302]
[33303]
[33304]
[33305]
TS
TT
TU
TV
2014 - Version 1-13
2008 Aug 27
2008 Sep 25
2008 Oct 19
2008 Sep 18
2008 Sep 22
(Compiled 2006)
Date of
orbital
Determination
Orbital
Inclination
(deg)
2008 Aug 29.33
65.02
2008 Aug 26.98
Nodal
period
(min)
Extra Page 2006 -15
Semi
major axis
(km)
Perigee
height
(km)
Apogee
height
(km)
Orbital
eccentric.
Argument
of perigee
(deg)
89.32 6619
230
252
0.002
219
65.06
89.08 6607
215
242
0.002
238
2008 Sep 25.05
64.99
89.07 6607
218
238
0.002
271
2008 Oct 17.67
65.06
92.10 6756
372
382
0.0008
252
2008 Aug 28.04
65.03
89.50 6628
238
261
0.002
237
2008 Aug 28.35
65.06
89.12 6610
222
240
0.001
217
2008 Nov 4.43
64.97
89.12 6609
227
234
0.0005
197
2008 Oct 20.35
64.96
89.05 6606
218
237
0.001
356
2008 Oct 19.66
65.07
89.87 6646
257
278
0.002
303
2008 Sep 25.99
64.94
90.02 6654
264
286
0.002
252
2008 Oct 29.49
65.02
89.57 6632
248
258
0.0007
323
2008 Sep 9.12
64.98
89.87 6647
255
281
0.002
231
2008 Sep 21.10
65.02
89.88 6647
255
283
0.002
253
2008 Sep 15.05
64.91
90.18 6662
268
300
0.002
216
2008 Aug 29.95
65.02
89.80 6643
251
277
0.002
222
2008 Sep 26.03
65.01
89.40 6623
232
257
0.002
268
794 days
823 days
847 days
816 days
820 days
RAE Table of Earth Satellites
Year of Launch 2006
Cospar ID
[Norad number]
Descent date
Lifetime
D
2006-26
2006-26
2006-26
2006-26
2006-26
2006-26
2006-26
TW
TX
TY
TZ
UA
UB
UC
[33306]
[33307]
[33308]
[33309]
[33310]
[33311]
[33348]
2008 Oct 7
835 days
D
2006-26 UD
2006-26 UE
[33349]
[33350]
2008 Nov 4
863 days
D
2006-26
2006-26
2006-26
2006-26
2006-26
UF
UG
UH
UJ
UK
[33351]
[33352]
[33353]
[33354]
[33355]
2008 Nov 7
866 days
D
2006-26 UL
2006-26 UM
2006-26 UN
[33356]
[33357]
[33358]
2008 Oct 8
836 days
D
2006-26
2006-26
2006-26
2006-26
UP
UQ
UR
US
[33359]
[33360]
[33361]
[33362]
2008 Oct 2
830 days
D
2006-26
2006-26
2006-26
2006-26
2006-26
UT
UU
UV
UW
UX
[33363]
[33364]
[33365]
[33366]
[33367]
2008 Oct 15
843 days
D
2006-26 UY
[33368]
2008 Oct 29
857 days
D
2006-26 UZ
[33369]
2008 Oct 22
850 days
D
2006-26 VA
2006-26 VB
[33370]
[33371]
2008 Oct 23
851 days
2006-26
2006-26
2006-26
2006-26
2006-26
2006-26
2006-26
2006-26
2006-26
2006-26
2006-26
[33416]
[33417]
[33418]
[33419]
[33420]
[33421]
[33422]
[33423]
[33424]
[33425]
[33426]
VC
VD
VE
VF
VG
VH
VJ
VK
VL
VM
VN
2014 - Version 1-13
(Compiled 2006)
Date of
orbital
Determination
Orbital
Inclination
(deg)
2008 Sep 22.08
64.99
2008
2008
2008
2008
2008
2008
2008
2008
2008
2008
2008
2008
2008
2008
2008
2008
2008
2008
2008
2008
2008
2008
2008
2008
2008
2008
2008
2008
2008
2008
2008
2008
2008
2008
2008
2008
2008
2008
2008
2008
2008
2008
2008
2008
64.97
64.96
65.01
65.09
65.08
65.02
65.08
65.01
65.01
65.10
65.09
65.04
65.08
65.06
65.07
65.09
65.09
64.98
65.02
65.00
65.00
65.04
65.04
65.00
65.05
65.04
64.99
64.99
65.07
65.06
65.08
65.09
65.10
65.00
65.13
65.03
64.99
65.02
65.01
65.02
65.03
64.99
65.05
65.08
Sep
Oct
Sep
Sep
Nov
Sep
Sep
Sep
Sep
Sep
Nov
Sep
Sep
Sep
Oct
Sep
Sep
Sep
Sep
Oct
Sep
Sep
Sep
Sep
Sep
Oct
Sep
Oct
Sep
Oct
Sep
Sep
Oct
Nov
Nov
Nov
Nov
Nov
Nov
Nov
Nov
Nov
Nov
Nov
15.09
7.47
15.69
15.55
4.43
15.55
15.10
15.70
15.09
14.68
6.39
15.71
15.27
17.70
5.50
15.69
15.67
15.70
15.63
2.24
15.71
15.69
15.75
15.64
15.64
15.42
15.70
28.25
15.67
22.71
15.08
15.09
22.31
3.50
1.10
3.50
3.46
3.66
3.19
3.71
3.40
3.07
3.63
3.52
Nodal
period
(min)
Extra Page 2006 -16
Semi
major axis
(km)
Perigee
height
(km)
Apogee
height
(km)
Orbital
eccentric.
Argument
of perigee
(deg)
89.53 6630
239
263
0.002
255
91.62
89.28
92.45
91.80
88.95
92.30
92.37
92.40
92.65
92.00
88.75
92.18
90.63
91.33
90.13
92.17
91.00
91.15
91.18
89.15
92.37
91.20
92.05
92.37
91.45
89.38
91.90
88.87
91.75
89.08
92.18
91.68
89.70
91.12
91.50
92.03
92.03
90.98
91.65
90.70
90.85
91.25
90.20
91.50
342
229
381
343
219
376
377
379
388
357
209
369
289
329
269
361
308
317
321
222
377
317
362
377
330
231
358
211
343
222
362
338
248
325
342
370
368
314
347
301
305
326
278
330
365
249
408
382
226
398
403
406
420
389
217
394
321
351
292
402
340
344
344
243
404
350
389
404
361
256
377
226
378
237
401
376
270
334
355
378
380
331
364
316
327
345
291
366
0.002
0.001
0.002
0.003
0.0005
0.002
0.002
0.002
0.002
0.002
0.0006
0.002
0.002
0.002
0.002
0.003
0.002
0.002
0.002
0.002
0.002
0.002
0.002
0.002
0.002
0.002
0.001
0.001
0.003
0.001
0.003
0.003
0.002
0.0007
0.001
0.0006
0.0009
0.001
0.001
0.001
0.002
0.001
0.001
0.003
213
303
226
284
1
270
233
226
214
240
236
255
264
257
329
285
263
224
241
310
217
246
269
223
247
310
217
351
269
315
278
273
310
299
237
194
255
291
269
295
302
273
325
287
6733
6618
6773
6741
6601
6766
6769
6771
6783
6752
6591
6760
6684
6719
6659
6760
6702
6709
6711
6611
6769
6712
6754
6769
6724
6623
6746
6597
6739
6608
6760
6735
6638
6708
6727
6753
6753
6701
6734
6687
6695
6714
6663
6726
RAE Table of Earth Satellites
Year of Launch 2006
Cospar ID
2006-26
2006-26
2006-26
2006-26
2006-26
2006-26
2006-26
2006-26
2006-26
2006-26
2006-26
2006-26
2006-26
2006-26
2006-26
2006-26
2006-26
[Norad number]
VP
VQ
VR
VS
VT
VU
VV
VW
VX
VY
VZ
WA
WB
WC
WD
WE
WF
Descent date
Lifetime
[33427]
[33428]
[33429]
[33430]
[33431]
[33432]
[33474]
[33475]
[33476]
[33477]
[33478]
[33479]
[33480]
[33481]
[33482]
[33483]
[33755]
SJ-8 CZ-2C 2nd stage fragments; 5 pieces, all have decayed
D 2006-35 C
[29387]
2006 Sep 13
4 days
D
2006-35 D
[29388]
2006 Sep 12
3 days
D
2006-35 E
[29389]
2006 Sep 12
3 days
D
2006-35 F
[29390]
2006 Sep 13
4 days
D
2006-35 G
[29392]
2006 Sep 12
3 days
IGS-O 2 H2A 2nd stage fragments; 12 pieces, all have decayed.
D 2006-37 C
[29395]
2006 Nov 7
57 days
D
[29396]
2007 Apr 26
227 days
[29493]
2007 Jun 29
291 days
D
D
D
2006-37 D
(Fairing halve)
2006-37 E
(Fairing halve)
2006-37 F
2006-37 G
2006-37 H
[32009]
[32010]
[32011]
2007 Aug 16
2007 Aug 5
2007 Aug 26
339 days
328 days
349 days
D
D
D
D
D
2006-37
2006-37
2006-37
2006-37
2006-37
[32012]
[32013]
[32014]
[32015]
[32016]
2007
2007
2007
2007
2007
337
338
330
342
348
D
J
K
L
M
N
2014 - Version 1-13
Aug
Aug
Aug
Aug
Aug
14
15
7
19
25
days
days
days
days
days
(Compiled 2006)
Nodal
period
(min)
Extra Page 2006 -17
Date of
orbital
Determination
Orbital
Inclination
(deg)
Semi
major axis
(km)
Perigee
height
(km)
Apogee
height
(km)
Orbital
eccentric.
Argument
of perigee
(deg)
2008
2008
2008
2008
2008
2008
Nov
Nov
Nov
Oct
Nov
Nov
3.43
3.45
3.51
31.11
3.49
3.63
64.98
64.98
65.07
65.01
65.03
65.09
91.75
92.05
92.27
91.58
90.63
90.73
6739
6753
6764
6731
6684
6689
355
368
371
345
298
299
366
381
400
359
313
322
0.0008
0.001
0.002
0.001
0.001
0.002
261
251
282
274
290
298
2006
2006
2006
2006
2006
2006
2006
2006
2006
2006
Sep
Sep
Sep
Sep
Sep
Sep
Sep
Sep
Sep
Sep
9.46
10.90
9.40
12.38
9.40
12.46
9.40
13.15
9.79
12.39
62.91
62.92
63.24
63.22
62.68
62.69
62.73
62.71
63.29
63.28
90.65
89.15
92.68
89.57
93.00
90.00
93.08
89.12
92.48
89.98
6685
6611
6785
6632
6800
6653
6804
6610
6775
6652
177
168
181
162
179
165
175
154
178
165
436
296
631
344
663
383
675
308
615
382
0.019
0.010
0.033
0.014
0.036
0.016
0.037
0.012
0.032
0.016
144
144
157
158
148
148
145
144
153
154
2006
2006
2006
2006
2006
2006
2007
2007
2007
2007
2007
2007
2007
2007
2007
2007
Sep
Oct
Sep
Oct
Sep
Oct
Aug
Aug
Aug
Aug
Aug
Jul
Jul
Aug
Aug
Aug
14.76
4.38
15.41
4.12
28.78
4.00
11.25
1.28
1.27
18.85
12.32
30.55
30.29
1.27
13.81
22.86
97.21
97.20
97.22
97.22
97.23
97.23
97.25
97.24
97.23
97.23
97.27
97.24
97.25
97.24
97.23
97.20
93.97
93.57
93.83
93.77
93.83
93.82
91.85
92.28
93.48
92.43
91.30
93.13
92.92
93.70
92.98
91.02
6847
6828
6840
6837
6840
6839
6744
6765
6823
6772
6717
6806
6796
6834
6799
6703
453
430
430
429
430
430
337
357
403
363
326
398
392
429
389
294
484
468
493
488
493
492
393
415
486
424
351
458
443
482
453
356
0.002
0.003
0.005
0.004
0.005
0.004
0.004
0.004
0.006
0.004
0.002
0.004
0.004
0.004
0.005
0.005
348
278
22
312
332
312
283
318
294
229
318
332
330
287
259
285
RAE Table of Earth Satellites
Year of Launch 2006
Cospar ID
D
[Norad number]
2006-37 P
[32017]
Descent date
Lifetime
2007 Aug 19
342 days
Cosmos 2423 fragments; 31 pieces, 30 have decayed
2006-39 C
[29397]
D 2006-39 D
[29604]
2006 Nov 18
D 2006-39 E
[29605]
2006 Nov 18
D 2006-39 F
[29606]
2006 Nov 20
65 days
65 days
67 days
D
D
D
2006-39 G
2006-39 H
2006-39 J
[29607]
[29608]
[29609]
2006 Nov 19
2006 Nov 18
2006 Nov 25
66 days
65 days
72 days
D
2006-39 K
[29610]
2006 Nov 23
70 days
D
D
D
D
2006-39
2006-39
2006-39
2006-39
L
M
N
P
[29611]
[29612]
[29613]
[29614]
2006
2006
2006
2006
65
67
65
67
D
D
2006-39 Q
2006-39 R
[29615]
[29616]
2006 Nov 18
2006 Nov 19
65 days
66 days
D
2006-39 S
[29617]
2006 Nov 24
71 days
D
D
2006-39 T
2006-39 U
[29618]
[29619]
2006 Nov 25
2007 Jan 6
72 days
114 days
D
D
2006-39 V
2006-39 W
[29620]
[29621]
2006 Nov 18
2006 Nov 24
65 days
71 days
D
D
2006-39 X
2006-39 Y
[29622]
[29623]
2006 Nov 18
2006 Nov 20
65 days
67 days
D
D
D
D
2006-39
2006-39
2006-39
2006-39
Z
AA
AB
AC
[29624]
[29625]
[29626]
[29627]
2006
2006
2006
2006
65
65
65
68
D
2006-39 AD
[29628]
2006 Nov 25
72 days
D
2006-39 AE
[29629]
2006 Nov 21
68 days
D
2006-39 AF
[29630]
2006 Nov 23
70 days
D
2006-39 AG
[29631]
2006 Dec 4
81 days
D
D
2006-39 AH
2006-39 AJ
[29634]
[29635]
2006 Nov 29
2006 Nov 30
76 days
77 days
2014 - Version 1-13
Nov
Nov
Nov
Nov
Nov
Nov
Nov
Nov
18
20
18
20
18
18
18
21
days
days
days
days
days
days
days
days
(Compiled 2006)
Date of
orbital
Determination
Orbital
Inclination
(deg)
2007 Aug 12.31
2007 Aug 18.85
97.25
97.17
2006
2006
2006
2006
2006
2006
2006
2006
2006
2006
2006
2006
2006
2006
2006
2006
2006
2006
2006
2006
2006
2006
2006
2007
2006
2006
2006
2006
2006
2006
2006
2006
2006
2006
2006
2006
2006
2006
2006
2006
2006
2006
2006
2006
2006
2006
64.91
64.72
65.06
64.78
64.77
64.75
64.77
64.51
64.49
64.69
64.70
64.76
64.79
64.81
64.81
64.81
64.87
64.72
64.71
64.83
64.81
64.70
64.83
64.76
65.04
65.09
65.06
64.77
65.03
65.10
65.10
64.71
65.03
64.71
64.70
64.71
64.65
64.76
64.72
64.96
64.94
64.40
64.40
65.24
65.17
65.15
Sep
Nov
Nov
Nov
Nov
Nov
Nov
Nov
Nov
Nov
Nov
Nov
Nov
Nov
Nov
Nov
Nov
Nov
Nov
Nov
Nov
Nov
Nov
Jan
Nov
Nov
Nov
Nov
Nov
Nov
Nov
Nov
Nov
Nov
Nov
Nov
Nov
Nov
Nov
Nov
Nov
Nov
Nov
Nov
Nov
Nov
15.00
18.23
18.48
18.49
20.18
18.41
18.48
18.72
25.14
18.72
23.34
18.23
18.60
18.50
18.48
19.52
18.48
18.49
19.49
18.45
23.15
18.48
18.06
6.78
18.23
18.71
24.42
18.23
18.49
20.12
18.23
18.23
18.54
18.45
21.15
18.46
24.43
18.46
21.42
18.46
23.19
18.46
29.36
28.34
28.37
30.34
Nodal
period
(min)
Extra Page 2006 -18
Semi
major axis
(km)
Perigee
height
(km)
Apogee
height
(km)
Orbital
eccentric.
Argument
of perigee
(deg)
92.90 6795
90.32 6669
382
263
451
318
0.005
0.004
264
301
88.58
88.88
89.03
90.72
88.60
88.70
88.55
94.15
89.70
94.17
90.42
89.32
88.72
88.63
88.73
87.83
89.28
90.42
89.52
94.13
90.88
89.40
94.20
95.42
88.52
93.93
89.17
88.92
90.75
88.38
88.88
88.55
89.23
94.10
90.05
95.05
91.22
94.68
89.92
95.20
90.98
95.00
89.55
90.82
92.52
90.27
160
182
180
195
164
177
174
194
170
185
173
183
187
175
185
149
186
194
175
193
177
174
197
205
163
194
168
171
192
155
180
165
189
178
158
188
169
175
158
193
179
189
161
182
188
173
248
257
274
425
247
243
232
760
349
771
416
299
235
238
240
186
292
395
326
760
459
315
762
873
240
740
298
270
431
234
258
241
284
772
395
853
500
831
383
863
467
848
342
447
607
402
0.007
0.006
0.007
0.017
0.006
0.005
0.004
0.041
0.013
0.043
0.018
0.009
0.004
0.005
0.004
0.003
0.008
0.015
0.011
0.041
0.021
0.011
0.041
0.048
0.006
0.040
0.010
0.007
0.018
0.006
0.006
0.006
0.007
0.043
0.018
0.048
0.025
0.048
0.017
0.048
0.022
0.048
0.014
0.020
0.031
0.017
66
94
126
127
110
134
135
115
114
108
105
101
122
95
117
133
141
121
117
113
111
113
115
91
152
116
107
148
113
107
122
104
125
104
102
110
102
103
101
114
109
111
111
115
118
114
6583
6598
6605
6688
6584
6589
6582
6856
6638
6857
6673
6619
6590
6585
6591
6546
6618
6673
6629
6855
6696
6623
6858
6917
6580
6845
6612
6599
6690
6573
6598
6581
6615
6853
6655
6899
6713
6881
6649
6907
6701
6897
6631
6693
6776
6666
RAE Table of Earth Satellites
Year of Launch 2006
Cospar ID
[Norad number]
Descent date
Lifetime
M-5 3rd stage fragments; 7 pieces, 6 have decayed
D 2006-41 C
[29481]
2006 Oct 11
19 days
D
2006-41 E
[29483]
2006 Oct 13
21 days
D
2006-41 G
[29485]
2006 Oct 15
23 days
D
2006-41 H
[29490]
2006 Oct 21
29 days
D
2006-41 J
[29491]
2006 Oct 3
11 days
D
2006-41 K
2006-41 L
[29492]
[31390]
2007 Nov 13
417 days
SJ 6-2A+B CZ-4B2 3rd stage fragments; 8 pieces, 1 has decayed
2006-46 D
[29508]
2006-46 E
[29509]
2006-46 F
[29636]
2006-46 G
[35374]
2006-46 H
[35375]
2006-46 J
[35376]
D 2006-46 K
[35377]
2013 Jan 18
2279 days
2006-46 L
Perigee
height
(km)
Apogee
height
(km)
Orbital
eccentric.
Argument
of perigee
(deg)
2006
2006
2006
2006
2006
2006
2006
2006
2006
2006
2006
2007
2007
23.99
10.99
23.01
13.00
25.55
15.55
26.01
18.81
26.78
2.80
27.54
10.62
13.32
98.32
98.27
98.31
98.28
98.32
98.31
98.37
98.31
98.34
98.32
98.37
98.29
98.25
94.07
89.53
93.70
90.02
93.72
88.62
93.73
91.70
93.18
89.43
92.13
93.22
89.43
6852
6630
6834
6654
6834
6584
6836
6736
6809
6625
6758
6811
6625
280
208
281
244
276
193
278
252
273
215
264
274
211
667
295
631
307
635
219
939
464
588
277
495
590
281
0.028
0.007
0.026
0.005
0.026
0.002
0.026
0.016
0.023
0.005
0.017
0.023
0.005
126
71
234
64
120
66
119
315
117
85
114
45
76
2006 Oct 24.09
2006 Oct 24.16
2006 Nov 28.00
97.63
97.72
97.75
96.58 6974
96.65 6977
96.97 6992
586
596
526
604
601
701
0.001
0.0004
0.013
293
81
232
2013 Jan 18.35
97.60
89.65 6635
244
269
0.002
130
Nov 5.97
Nov 4.98
98.78
98.82
101.85 7225
101.77 7221
845
823
848
862
0.0002
0.003
7
13
Nov
Nov
Nov
Nov
Aug
Nov
Nov
Nov
Nov
Nov
Nov
Nov
Nov
Nov
Nov
Nov
Nov
Nov
Nov
Nov
98.52
98.50
98.51
98.51
98.52
98.83
98.66
98.81
98.78
98.81
98.83
98.94
98.67
98.83
98.53
99.02
98.82
98.77
98.89
98.84
99.63
92.92
90.95
97.98
89.72
101.57
100.37
101.60
101.55
101.57
101.58
100.55
100.60
100.68
100.80
100.75
100.90
101.10
101.15
101.48
636
327
277
487
239
817
699
819
814
819
819
718
714
718
737
739
754
772
774
811
846
507
366
838
282
849
853
849
849
847
849
851
860
864
856
849
849
850
852
847
0.015
0.013
0.007
0.025
0.0032
0.002
0.011
0.002
0.002
0.002
0.002
0.009
0.010
0.010
0.008
0.008
0.007
0.005
0.005
0.002
317
303
276
331
148
320
305
349
358
324
329
347
291
286
298
347
314
351
357
332
Sep
Oct
Sep
Oct
Sep
Oct
Sep
Oct
Sep
Oct
Sep
May
Nov
Nodal
period
(min)
Extra Page 2006 -19
Orbital
Inclination
(deg)
Semi
major axis
(km)
[35378]
Delta-4 2nd stage fragments; 68 pieces, 5 have decayed.
2006-50 C
[29524]
2006
2006-50 D
[29525]
2006
Fragments C and D are the instrument covers of the Operational Linescan System.
2006-50 E
[29540]
2006
D 2006-50 F
[29541]
2006 Nov 16
12 days
2006
2006
D 2006-50 G
[29542]
2007 Aug 4
273 days
2006
2007
2006-50 H
[29543]
2006
2006-50 J
[29544]
2006
2006-50 K
[29545]
2006
2006-50 L
[29546]
2006
2006-50 M
[29547]
2006
2006-50 N
[29548]
2006
2006-50 P
[29549]
2006
2006-50 Q
[29550]
2006
2006-50 R
[29551]
2006
2006-50 S
[29552]
2006
2006-50 T
[29553]
2006
2006-50 U
[29554]
2006
2006-50 V
[29555]
2006
2006-50 W
[29556]
2006
2006-50 X
[29557]
2006
2014 - Version 1-13
(Compiled 2006)
Date of
orbital
Determination
13.70
14.07
15.99
13.82
4.54
14.01
14.39
14.02
14.02
13.87
13.94
13.99
13.99
14.00
14.01
14.01
14.02
13.97
13.97
13.86
7119
6796
6700
7041
6639
7212
7154
7213
7210
7211
7212
7163
7166
7170
7175
7173
7180
7190
7191
7207
RAE Table of Earth Satellites
Year of Launch 2006
Cospar ID
[Norad number]
Lifetime
2006
2006
2006
2006
2006
2006
2006
2006
2006
2006
2006
2006
2006
2006
2006
2006
2006
2006
2006
2006
2006
2006
2006
2006
2006
2006
2006
2006
2006
2006
2006
2006
2006
2006
2006
2006
2006
2006
2006
2006
2006
2006
2006
Nov
Nov
Nov
Nov
Nov
Nov
Nov
Nov
Nov
Nov
Nov
Nov
Nov
Nov
Nov
Nov
Nov
Nov
Nov
Nov
Nov
Nov
Nov
Nov
Nov
Nov
Nov
Nov
Nov
Nov
Nov
Nov
Nov
Nov
Nov
Nov
Nov
Nov
Nov
Nov
Nov
Nov
Nov
13.88
14.04
14.00
14.02
14.02
13.88
13.88
13.87
14.00
13.87
13.89
13.97
13.87
13.94
13.96
14.02
14.03
14.06
13.93
13.99
14.05
14.06
13.97
14.04
13.96
14.05
13.94
14.05
13.91
14.03
14.11
14.05
13.92
13.92
13.94
13.94
13.98
14.10
14.14
14.01
14.01
13.91
17.51
98.81
98.80
99.11
98.56
98.90
98.79
98.81
98.57
98.63
98.71
98.75
98.64
98.69
98.80
98.76
98.71
98.82
98.74
98.63
98.61
98.81
98.84
98.76
98.74
98.75
98.72
98.67
98.73
98.61
98.87
98.78
98.78
98.81
98.77
98.82
98.80
98.69
98.75
98.78
98.75
98.79
98.82
98.79
101.67
101.05
99.93
100.07
100.88
101.63
101.62
96.42
99.98
100.03
100.18
100.35
100.80
100.77
101.02
100.90
100.95
100.52
99.87
101.27
101.27
101.35
101.05
101.12
100.98
101.18
99.98
100.43
100.35
101.02
101.07
101.18
101.32
101.32
101.53
101.58
100.42
101.02
101.42
101.50
101.52
101.57
101.88
Nov
Aug
Nov
Nov
100.28
93.72
100.32
101.88
D
[29632]
2007 Aug 9
278 days
28.50
27.05
26.95
29.93
98.88
98.99
98.85
98.78
D
2006-50 BU
[29633]
2006-50 BV
[29637]
DMSP 5D-3 fragment
2006-50 BW
[29708]
2006
2007
2006
2006
2007 Aug 5
274 days
2007 Jan 7.97
2007 Feb 11.53
98.62
98.57
2014 - Version 1-13
2006 Dec 1
27 days
Nodal
period
(min)
Extra Page 2006 -20
Orbital
Inclination
(deg)
2006-50 Y
2006-50 Z
2006-50 AA
2006-50 AB
2006-50 AC
2006-50 AD
2006-50 AE
2006-50 AF
2006-50 AG
2006-50 AH
2006-50 AJ
2006-50 AK
2006-50 AL
2006-50 AM
2006-50 AN
2006-50 AP
2006-50 AQ
2006-50 AR
2006-50 AS
2006-50 AT
2006-50 AU
2006-50 AV
2006-50 AW
2006-50 AX
2006-50 AY
2006-50 AZ
2006-50 BA
2006-50 BB
2006-50 BC
2006-50 BD
2006-50 BE
2006-50 BF
2006-50 BG
2006-50 BH
2006-50 BJ
2006-50 BK
2006-50 BL
2006-50 BM
2006-50 BN
2006-50 BP
2006-50 BQ
2006-50 BR
2006-50 BS
DMSP 5D-3 fragment
2006-50 BT
D
[29558]
[29559]
[29560]
[29561]
[29562]
[29563]
[29564]
[29565]
[29566]
[29567]
[29568]
[29569]
[29570]
[29571]
[29572]
[29573]
[29574]
[29575]
[29576]
[29577]
[29578]
[29579]
[29580]
[29581]
[29582]
[29583]
[29584]
[29585]
[29586]
[29587]
[29588]
[29589]
[29590]
[29591]
[29592]
[29593]
[29594]
[29595]
[29596]
[29597]
[29598]
[29599]
[29600]
Descent date
(Compiled 2006)
Date of
orbital
Determination
Semi
major axis
(km)
Perigee
height
(km)
Apogee
height
(km)
Orbital
eccentric.
Argument
of perigee
(deg)
7216
7187
7134
7140
7179
7215
7214
6966
7136
7139
7146
7154
7175
7173
7186
7180
7182
7162
7131
7197
7197
7201
7187
7190
7183
7193
7136
7158
7158
7186
7188
7193
7200
7199
7210
7212
7157
7185
7204
7208
7209
7211
7226
829
768
666
676
750
821
821
372
664
673
684
700
733
741
766
752
755
715
658
776
785
793
767
771
755
775
668
698
704
765
769
775
790
790
811
820
703
765
791
799
814
814
841
847
849
845
848
850
851
849
802
850
848
850
851
859
848
849
850
853
852
847
861
852
852
849
852
855
854
847
861
855
850
849
854
852
851
852
847
853
848
860
860
847
851
854
0.001
0.006
0.013
0.012
0.007
0.002
0.002
0.031
0.013
0.012
0.012
0.011
0.009
0.007
0.006
0.007
0.007
0.010
0.013
0.006
0.005
0.004
0.006
0.006
0.007
0.005
0.013
0.011
0.011
0.006
0.006
0.005
0.004
0.004
0.003
0.002
0.010
0.006
0.005
0.004
0.002
0.003
0.0009
347
307
331
334
350
7
352
266
310
311
308
302
289
313
346
348
305
306
323
15
351
2
306
306
296
289
317
295
299
340
348
289
292
309
353
345
301
306
20
271
341
6
224
7150
6835
7152
7226
690
428
704
841
854
485
844
854
0.011
0.004
0.010
0.0009
317
160
267
187
98.32 7057
97.80 7032
591
573
766
735
0.012
0.012
145
13
RAE Table of Earth Satellites
Year of Launch 2006
Cospar ID
2006-50 BX
[Norad number]
Descent date
Lifetime
Date of
orbital
Determination
(Compiled 2006)
Orbital
Inclination
(deg)
Nodal
period
(min)
Extra Page 2006 -21
Semi
major axis
(km)
Perigee
height
(km)
Apogee
height
(km)
Orbital
eccentric.
Argument
of perigee
(deg)
[35421]
USA-193 fragments, 173 pieces, 103 have decayed
Satellite malfunctioned shortly after launch and stayed in low parking orbit. An Aegis-SM3 missile from warship USS Lake Erie hit the satellite 2008 Feb
20.143 and destroyed it.
D
2006-57 C
[32502]
2008 Mar 1
443 days
D
2006-57 D
2006-57 E
[32503]
[32504]
2008 Mar 1
443 days
D
2006-57 F
2006-57 G
[32505]
[32506]
2008 Feb 29
442 days
D
2006-57 H
2006-57 J
[32507]
[32508]
2008 Mar 7
449 days
D
2006-57 K
2006-57 L
2006-57 M
[32509]
[32510]
[32511]
2008 Mar 7
449 days
D
2006-57 N
2006-57 P
[32512]
[32513]
2008 Feb 27
440 days
D
2006-57 Q
[32514]
2008 Mar 2
444 days
D
2006-57 R
[32515]
2008 Apr 3
476 days
D
2006-57 S
[32516]
2008 Mar 1
443 days
D
2006-57 T
[32517]
2008 Mar 17
459 days
D
2006-57 U
[32518]
2008 Mar 2
444 days
D
2006-57 V
[32519]
2008 Mar 13
455 days
D
2006-57 W
[32520]
2008 Mar 1
443 days
D
2006-57 X
[32521]
2008 Mar 17
459 days
D
2006-57 Y
[32522]
2008 Mar 17
459 days
D
2006-57 Z
[32523]
2008 Mar 12
454 days
D
2006-57 AA
2006-57 AB
2006-57 AC
[32524]
[32525]
[32526]
2008 Mar 3
445 days
2006-57 AD
2006-57 AE
2006-57 AF
[32527]
[32528]
[32529]
2014 - Version 1-13
2008
2008
2008
2008
2008
2008
2008
2008
2008
2008
2008
2008
2008
2008
2008
2008
2008
2008
2008
2008
2008
2008
2008
2008
2008
2008
2008
2008
2008
2008
2008
2008
2008
2008
2008
2008
2008
2008
2008
2008
2008
2008
2008
2008
2008
Feb
Feb
Feb
Feb
Mar
Feb
Feb
Feb
Feb
Feb
Mar
Feb
Feb
Feb
Mar
Feb
Feb
Feb
Feb
Mar
Feb
Apr
Feb
Mar
Feb
Mar
Feb
Mar
Feb
Mar
Feb
Mar
Mar
Mar
Mar
Mar
Mar
Mar
Feb
Feb
Feb
Mar
Feb
Feb
Feb
26.27
29.99
26.78
26.68
1.06
26.74
26.76
29.34
26.76
26.32
5.93
26.66
26.66
26.70
7.13
26.79
26.72
27.09
26.78
2.22
26.68
3.43
26.22
1.21
26.42
14.73
26.16
1.78
27.91
13.77
27.86
1.03
3.19
14.74
3.18
14.03
3.75
10.74
27.81
27.68
27.73
2.06
27.72
27.72
27.75
57.24
57.33
58.29
57.95
57.87
58.42
58.82
58.75
58.68
58.37
58.38
58.23
58.55
58.45
58.35
58.55
57.81
57.82
58.47
58.47
58.73
58.70
58.36
58.33
59.23
59.23
58.51
58.48
58.46
58.40
58.71
58.71
58.63
58.62
59.28
59.19
56.54
56.53
58.81
58.51
59.38
59.38
58.12
58.02
58.35
100.85
90.23
106.00
93.97
88.10
102.80
94.47
90.22
103.38
97.15
91.07
100.13
95.68
94.47
89.05
96.70
89.03
88.12
89.08
87.78
94.72
89.00
96.23
90.32
92.45
88.72
90.83
88.00
98.90
89.77
89.18
88.03
98.08
90.00
96.80
88.83
91.77
88.42
99.95
92.95
91.35
88.35
92.73
92.68
93.87
7178
6664
7420
6847
6559
7270
6871
6664
7297
7001
6705
7143
6930
6871
6606
6979
6606
6560
6608
6543
6884
6603
6957
6669
6773
6589
6694
6554
7084
6642
6612
6556
7046
6653
6984
6595
6739
6575
7135
6797
6720
6577
6787
6785
6842
166
144
213
172
140
227
171
149
229
235
200
240
242
226
179
239
195
171
202
153
243
183
192
157
239
188
188
149
218
166
217
173
229
194
235
183
233
179
238
239
219
174
236
242
239
1432
428
1869
765
220
1554
813
421
1608
1009
453
1290
861
759
275
962
259
191
256
176
767
267
964
423
549
233
443
202
1193
360
250
181
1105
355
975
250
488
212
1274
599
463
223
581
570
687
0.088
0.021
0.112
0.043
0.006
0.091
0.047
0.020
0.094
0.055
0.019
0.073
0.045
0.039
0.007
0.052
0.005
0.002
0.004
0.002
0.038
0.006
0.055
0.020
0.023
0.003
0.019
0.004
0.069
0.015
0.003
0.0006
0.062
0.012
0.053
0.005
0.019
0.003
0.073
0.026
0.018
0.004
0.025
0.024
0.033
63
73
15
2
6
18
1
10
45
24
40
26
40
14
7
43
12
20
307
299
35
82
6
9
26
25
346
346
16
47
41
85
52
78
34
36
64
114
42
45
60
77
52
33
44
RAE Table of Earth Satellites
Year of Launch 2006
Cospar ID
[Norad number]
Descent date
Lifetime
D
2006-57
2006-57
2006-57
2006-57
AG
AH
AJ
AK
[32530]
[32531]
[32532]
[32533]
2008 Mar 2
444 days
D
2006-57 AL
[32534]
2008 Mar 17
459 days
D
2006-57 AM
[32535]
2008 Mar 7
449 days
D
2006-57 AN
[32536]
2008 Mar 5
447 days
D
2006-57 AP
[32537]
2008 Mar 2
444 days
D
2006-57 AQ
2006-57 AR
[32538]
[32539]
2008 Mar 14
456 days
D
2006-57 AS
2006-57 AT
[32540]
[32541]
2008 Mar 5
447 days
D
2006-57 AU
2006-57 AV
2006-57 AW
[32542]
[32543]
[32544]
2008 Mar 7
449 days
D
2006-57 AX
2006-57 AY
[32545]
[32546]
2008 Mar 1
443 days
D
2006-57 AZ
2006-57 BA
2006-57 BB
[32578]
[32579]
[32580]
2008 Mar 17
459 days
D
2006-57 BC
2006-57 BD
[32581]
[32582]
2008 Apr 8
481 days
D
2006-57 BE
[32583]
2008 Apr 6
479 days
D
2006-57 BF
[32584]
2008 Mar 7
449 days
D
2006-57 BG
[32585]
2008 Mar 7
449 days
D
2006-57 BH
[32586]
2008 Mar 13
455 days
D
2006-57 BJ
[32587]
2008 Mar 5
447 days
D
2006-57 BK
[32588]
2008 Mar 8
450 days
D
2006-57 BL
2006-57 BM
[32589]
[32590]
2008 Mar 24
466 days
D
2006-57 BN
[32591]
2008 Apr 12
485 days
D
2006-57 BP
[32592]
2008 Mar 14
456 days
2014 - Version 1-13
(Compiled 2006)
Nodal
period
(min)
Extra Page 2006 -22
Date of
orbital
Determination
Orbital
Inclination
(deg)
Semi
major axis
(km)
2008
2008
2008
2008
2008
2008
2008
2008
2008
2008
Feb
Feb
Feb
Feb
Mar
Feb
Mar
Feb
Mar
Feb
27.49
27.76
28.83
28.84
2.21
28.87
17.38
28.22
6.93
28.27
58.27
58.20
58.51
58.67
58.65
58.31
58.30
60.39
60.38
59.28
91.37
91.57
115.03
90.28
88.63
90.40
87.70
94.43
89.68
91.80
2008
2008
2008
2008
2008
2008
2008
2008
2008
2008
2008
2008
2008
2008
2008
2008
2008
2008
2008
2008
2008
2008
2008
2008
2008
2008
2008
2008
2008
2008
2008
2008
2008
2008
2008
2008
2008
2008
2008
2008
Feb
Mar
Feb
Feb
Mar
Feb
Feb
Mar
Feb
Feb
Feb
Mar
Feb
Feb
Mar
Feb
Feb
Mar
Mar
Feb
Feb
Apr
Feb
Apr
Mar
Mar
Feb
Mar
Feb
Mar
Feb
Mar
Mar
Mar
Mar
Mar
Mar
Mar
Apr
Mar
28.84
2.17
28.84
28.78
10.96
28.18
28.20
4.13
28.93
28.21
28.18
7.11
28.94
28.86
1.17
29.76
29.21
1.00
15.00
29.97
29.98
8.65
29.99
6.90
1.00
7.51
29.99
5.97
29.22
11.95
29.98
4.19
3.93
8.04
3.91
3.87
21.80
3.89
12.18
3.84
58.28
58.26
58.65
58.70
58.69
58.63
58.88
58.88
58.91
58.69
58.80
58.77
58.16
58.95
58.96
58.40
58.65
58.18
58.17
58.45
58.63
58.65
59.12
59.15
58.57
58.54
58.34
58.34
58.92
58.92
58.52
58.51
57.43
57.32
59.58
58.30
58.59
59.58
59.58
58.54
91.35
89.73
92.98
92.77
89.17
93.52
93.58
89.82
95.65
96.80
90.90
88.35
91.13
90.67
89.38
89.95
89.25
91.40
88.45
94.62
107.18
88.57
109.32
88.92
88.95
87.45
90.43
88.82
91.92
88.38
89.22
88.03
98.25
92.10
96.37
89.22
87.73
107.72
89.42
97.50
Perigee
height
(km)
Apogee
height
(km)
Orbital
eccentric.
Argument
of perigee
(deg)
6720
6730
7836
6667
6585
6672
6540
6870
6637
6741
242
234
226
225
181
240
154
234
203
223
441
469
2688
351
233
348
168
748
315
502
0.015
0.017
0.157
0.009
0.004
0.008
0.001
0.037
0.008
0.021
33
14
21
52
69
27
20
41
55
11
6719
6640
6799
6789
6612
6825
6828
6644
6928
6984
6697
6572
6709
6686
6623
6651
6616
6722
6576
6878
7475
6582
7574
6599
6601
6526
6674
6595
6747
6573
6614
6556
7053
6756
6963
6614
6541
7500
6624
7018
231
212
215
237
196
239
239
212
229
239
232
183
239
232
207
241
222
238
180
238
239
166
234
172
219
146
229
194
238
173
204
166
186
172
240
213
153
231
175
204
450
311
626
583
271
654
660
318
870
971
405
203
421
382
281
303
253
449
215
761
1953
241
2156
270
225
150
362
238
507
216
267
188
1164
582
929
268
171
2012
315
1074
0.016
0.007
0.030
0.026
0.006
0.030
0.031
0.008
0.046
0.052
0.013
0.001
0.014
0.011
0.006
0.005
0.002
0.016
0.003
0.038
0.115
0.006
0.127
0.007
0.0004
0.0003
0.010
0.003
0.021
0.003
0.005
0.002
0.070
0.030
0.049
0.003
0.001
0.119
0.011
0.062
31
39
6
46
58
25
38
58
17
45
18
52
37
34
32
54
121
35
54
46
41
51
41
69
6
304
52
73
56
83
337
319
21
36
38
325
329
43
79
20
RAE Table of Earth Satellites
Year of Launch 2006
Cospar ID
[Norad number]
Descent date
Lifetime
D
2006-57 BQ
2006-57 BR
2006-57 BS
[32593]
[32594]
[32595]
2008 Mar 22
464 days
D
2006-57 BT
2006-57 BU
[32596]
[32597]
2008 Apr 9
482 days
D
2006-57 BV
[32598]
2008 Mar 17
459 days
D
2006-57 BW
[32599]
2008 Mar 23
465 days
D
2006-57 BX
2006-57 BY
[32600]
[32601]
2008 Mar 30
472 days
D
2006-57 BZ
2006-57 CA
[32602]
[32603]
2008 Mar 12
454 days
D
2006-57 CB
2006-57 CC
[32604]
[32605]
2008 Apr 7
480 days
D
2006-57 CD
[32606]
2008 Apr 8
481 days
D
2006-57 CE
[32607]
2008 Mar 13
455 days
D
2006-57 CF
2006-57 CG
[32608]
[32609]
2008 Mar 12
454 days
D
2006-57 CH
[32610]
2008 Mar 5
447 days
D
2006-57 CJ
[32611]
2008 Mar 14
456 days
D
2006-57 CK
[32612]
2008 Apr 9
482 days
D
2006-57 CL
[32613]
2008 Mar 20
462 days
D
2006-57 CM
[32614]
2008 Mar 12
454 days
D
2006-57 CN
[32615]
2008 Mar 13
455 days
D
2006-57 CP
[32616]
2008 Mar 24
466 days
D
2006-57 CQ
[32617]
2008 Mar 4
456 days
D
2006-57 CR
[32618]
2008 Mar 8
450 days
D
2006-57 CS
2006-57 CT
2006-57 CU
[32619]
[32620]
[32621]
2008 Mar 11
453 days
2006-57 CV
[32622]
2014 - Version 1-13
(Compiled 2006)
Date of
orbital
Determination
Orbital
Inclination
(deg)
2008
2008
2008
2008
2008
2008
2008
2008
2008
2008
2008
2008
2008
2008
2008
2008
2008
2008
2008
2008
2008
2008
2008
2008
2008
2008
2008
2008
2008
2008
2008
2008
2008
2008
2008
2008
2008
2008
2008
2008
2008
2008
2008
2008
2008
2008
2008
2008
2008
2008
2008
58.50
58.49
58.77
58.65
58.64
58.23
58.67
58.69
58.23
58.26
59.13
59.12
59.42
58.54
58.50
57.20
58.71
58.66
58.50
58.61
58.59
58.52
58.50
58.30
58.27
58.54
58.58
58.55
57.90
57.92
58.18
58.16
58.40
58.39
58.16
58.14
58.34
58.31
58.70
58.68
58.65
58.62
58.63
58.61
58.30
58.31
56.67
58.25
58.87
58.88
59.54
Mar
Mar
Mar
Mar
Mar
Mar
Mar
Apr
Mar
Mar
Mar
Mar
Mar
Mar
Aug
Mar
Mar
Mar
Mar
Mar
Apr
Mar
Apr
Mar
Mar
Mar
Mar
Mar
Mar
Mar
Mar
Mar
Mar
Apr
Mar
Mar
Mar
Mar
Mar
Mar
Mar
Mar
Mar
Mar
Mar
Mar
Mar
Mar
Mar
Mar
Mar
11.95
3.92
3.88
3.94
22.68
3.94
3.80
9.48
3.92
16.01
3.92
23.57
3.94
3.95
27.72
3.91
3.92
9.92
3.88
3.96
6.56
3.84
8.59
3.87
12.67
3.82
3.96
9.08
3.92
4.16
3.78
12.73
3.86
9.38
3.94
20.91
3.95
12.06
3.10
13.08
3.88
21.94
3.94
13.53
3.96
8.08
3.79
4.93
4.92
10.92
4.96
Nodal
period
(min)
Extra Page 2006 -23
Semi
major axis
(km)
90.90
96.93
97.30
97.57
88.50
90.12
108.38
88.62
96.45
88.80
96.95
88.25
95.92
96.82
88.87
96.60
94.48
88.82
95.80
93.45
88.58
94.68
89.10
89.10
87.07
90.38
89.43
87.50
88.55
87.80
90.13
87.62
91.07
87.43
91.42
88.88
89.68
87.87
89.80
88.00
89.27
87.45
89.10
87.17
89.02
87.47
94.33
104.42
97.10
91.10
95.97
6697
6991
7008
7021
6579
6659
7531
6585
6957
6594
6991
6567
6942
6985
6597
6974
6872
6595
6936
6822
6583
6882
6609
6608
6508
6672
6625
6529
6581
6544
6659
6535
6706
6526
6723
6598
6637
6548
6643
6554
6617
6527
6608
6513
6604
6527
6865
7346
6998
6707
6944
Perigee
height
(km)
Apogee
height
(km)
Orbital
eccentric.
Argument
of perigee
(deg)
170
238
235
236
170
211
242
181
209
177
236
167
236
241
183
243
200
148
240
228
168
239
180
208
123
235
206
143
191
125
227
146
238
141
233
190
230
164
231
169
230
144
183
124
203
143
235
211
223
207
238
467
986
1024
1049
230
349
2062
232
967
253
990
209
890
971
253
948
787
284
874
658
241
767
280
252
136
352
287
158
214
205
335
167
416
153
455
249
288
174
299
181
247
153
277
144
249
154
738
1723
1016
449
892
0.022
0.054
0.056
0.058
0.005
0.010
0.121
0.004
0.054
0.006
0.054
0.003
0.047
0.052
0.005
0.051
0.043
0.010
0.046
0.031
0.006
0.038
0.008
0.003
0.001
0.009
0.006
0.001
0.002
0.006
0.008
0.002
0.013
0.0009
0.017
0.004
0.004
0.0007
0.005
0.0009
0.001
0.0007
0.007
0.002
0.003
0.0008
0.037
0.103
0.057
0.018
0.047
29
50
48
47
100
356
40
82
24
65
40
52
33
48
310
47
18
34
49
22
47
47
87
117
168
16
358
3
71
177
66
79
31
69
29
59
51
57
44
54
5
309
122
146
343
285
60
23
54
58
41
RAE Table of Earth Satellites
Year of Launch 2006
Cospar ID
[Norad number]
Descent date
Lifetime
D
2006-57 CW
[32623]
2008 Mar 14
456 days
D
CX
CY
CZ
DA
[32624]
[32625]
[32626]
[32627]
2008 Mar 6
448 days
D
2006-57
2006-57
2006-57
2006-57
2008 Mar 12
454 days
D
2006-57 DB
2006-57 DC
2006-57 DD
[32628]
[32629]
[32630]
2008 Mar 12
454 days
[32631]
[32632]
[32633]
2008 Mar 6
448 days
D
2006-57 DE
2006-57 DF
2006-57 DG
2008 Mar 6
448 days
D
2006-57 DH
2006-57 DJ
[32634]
[32635]
2008 Mar 11
D
2006-57 DK
[32636]
2008 Mar 7
449 days
D
2006-57 DL
[32637]
2008 Mar 7
449 days
D
2006-57 DM
[32638]
2008 Mar 17
459 days
D
2006-57 DN
2006-57 DP
2006-57 DQ
[32639]
[32640]
[32641]
2008 Mar 7
449 days
D
2006-57 DR
[32642]
2008 Apr 11
484 days
D
2006-57 DS
[32643]
2008 Mar 8
450 days
D
D
DT
DU
DV
DW
DX
DY
[32644]
[32645]
[32646]
[32647]
[32648]
[32649]
2008 Mar 7
2008 Mar 6
449 days
448 days
D
D
D
2006-57
2006-57
2006-57
2006-57
2006-57
2006-57
2008 Mar 6
2008 Mar 6
2008 Mar 24
448 days
448 days
466 days
D
2006-57
2006-57
2006-57
2006-57
2006-57
DZ
EA
EB
EC
ED
[32650]
[32651]
[32652]
[32653]
[32654]
2008 Mar 17
459 days
D
2006-57 EE
[32655]
2008 Apr 9
482 days
D
2006-57 EF
2006-57 EG
[32656]
[32657]
2008 Oct 9
D
2006-57 EH
[32658]
2008 Mar 8
D
2014 - Version 1-13
450 days
(Compiled 2006)
Date of
orbital
Determination
Orbital
Inclination
(deg)
2008
2008
2008
2008
2008
2008
2008
2008
2008
2008
2008
2008
2008
2008
2008
2008
2008
2008
2008
2008
2008
2008
2008
2008
2008
2008
2008
2008
2008
2008
2008
2008
2008
2008
2008
2008
2008
2008
2008
2008
2008
2008
2008
2008
2008
2008
2008
2008
2008
2008
2008
60.35
60.32
58.27
57.65
58.38
58.32
58.31
58.75
58.07
58.40
58.40
58.86
58.75
60.42
60.41
58.27
58.72
58.70
57.44
57.43
58.59
58.54
58.33
58.31
57.95
55.81
58.93
58.51
56.50
56.50
58.26
58.26
59.75
58.18
57.47
58.34
58.64
58.34
58.33
58.22
58.63
58.95
58.96
59.35
59.36
57.92
57.91
56.70
57.69
57.62
59.39
Mar
Mar
Mar
Mar
Mar
Mar
Mar
Mar
Mar
Mar
Mar
Mar
Mar
Mar
Mar
Mar
Mar
Mar
Mar
Mar
Mar
Mar
Mar
Mar
Mar
Mar
Mar
Mar
Mar
Apr
Mar
Mar
Mar
Mar
Mar
Mar
Mar
Mar
Mar
Mar
Mar
Mar
Mar
Mar
Mar
Mar
Apr
Mar
Mar
Oct
Mar
4.78
11.95
4.57
4.81
4.95
4.96
9.06
4.81
4.90
4.88
10.07
4.21
4.82
4.96
5.97
4.92
4.80
9.66
4.84
5.95
4.81
7.10
4.74
16.66
4.76
4.73
4.74
6.86
5.10
11.20
5.28
8.02
5.06
4.94
5.55
4.86
5.08
5.83
19.80
5.82
4.93
5.19
5.16
5.17
15.03
5.12
9.55
5.75
5.16
8.70
5.16
Nodal
period
(min)
Extra Page 2006 -24
Semi
major axis
(km)
95.25
88.25
87.65
103.00
89.92
89.98
88.72
89.75
91.58
90.75
88.90
89.18
94.03
90.85
89.55
93.20
88.95
87.82
89.12
88.27
89.83
88.08
89.47
87.73
91.77
94.00
94.40
90.30
96.62
88.88
90.08
88.43
89.38
88.13
95.30
88.42
88.13
90.52
88.23
90.70
92.38
94.95
95.38
94.60
89.33
93.98
89.35
94.02
95.07
88.30
91.55
6909
6566
6536
7279
6649
6652
6589
6640
6731
6690
6599
6612
6850
6695
6631
6810
6601
6545
6609
6567
6644
6558
6627
6541
6740
6849
6868
6668
6975
6598
6657
6576
6623
6560
6912
6574
6561
6678
6566
6687
6770
6894
6916
6877
6620
6848
6621
6849
6901
6569
6729
Perigee
height
(km)
Apogee
height
(km)
Orbital
eccentric.
Argument
of perigee
(deg)
226
149
146
196
237
213
187
236
228
229
195
193
208
204
182
236
215
163
206
174
211
166
217
160
238
240
212
190
241
184
218
180
193
162
231
184
170
231
168
237
238
237
237
233
201
236
194
236
243
175
228
835
226
169
1605
305
334
234
288
477
394
245
274
736
429
323
627
230
169
255
203
321
192
279
165
485
701
766
387
952
255
339
214
295
202
835
207
194
368
206
381
545
795
837
765
282
702
291
705
801
207
473
0.044
0.006
0.002
0.097
0.005
0.009
0.004
0.004
0.019
0.012
0.004
0.006
0.039
0.017
0.011
0.029
0.001
0.0005
0.004
0.002
0.008
0.002
0.005
0.0004
0.018
0.034
0.040
0.015
0.051
0.005
0.009
0.003
0.008
0.003
0.044
0.002
0.002
0.010
0.003
0.011
0.023
0.040
0.043
0.039
0.006
0.034
0.007
0.034
0.010
0.002
0.018
24
13
330
24
87
16
22
47
71
44
60
32
14
57
61
54
74
52
21
6
69
96
94
85
43
59
54
61
52
131
59
62
28
173
32
17
1
63
69
26
31
45
45
47
65
328
71
65
43
90
39
RAE Table of Earth Satellites
Year of Launch 2006
Cospar ID
[Norad number]
Descent date
Lifetime
D
2006-57 EJ
[32659]
2008 Mar 17
459 days
D
2006-57 EK
2006-57 EL
[32660]
[32661]
2008 Mar 12
454 days
D
2006-57 EM
[32662]
2008 Mar 7
449 days
D
2006-57 EN
[32663]
2008 Mar 12
454 days
D
2006-57 EP
[32664]
2008 Apr 6
479 days
D
2006-57 EQ
2006-57 ER
[32665]
[32666]
2008 Mar 12
454 days
D
2006-57 ES
2006-57 ET
[32667]
[32668]
2008 Apr 2
475 days
D
2006-57 EU
2006-57 EV
2006-57 EW
[32669]
[32670]
[32671]
2008 Apr 9
485 days
D
2006-57 EX
[32672]
2008 Apr 3
476 days
`
EY
EZ
FA
FB
[32673]
[32674]
[32675]
[32676]
2008 Mar 7
449 days
D
2006-57
2006-57
2006-57
2006-57
2008 Mar 24
466 days
D
2006-57 FC
2006-57 FD
[32677]
[32678]
2008 Mar 14
456 days
D
2006-57 FE
2006-57 FF
2006-57 FG
[32679]
[32680]
[32681]
2008 Apr 2
475 days
D
2006-57 FH
[32682]
2008 Mar 24
466 days
D
2006-57 FJ
2006-57 FK
[32683]
[32684]
2008 Mar 17
459 days
D
2006-57 FL
2006-57 FM
[32685]
[32688]
2008 Mar 17
459 days
D
2006-57 FN
[32689]
2008 Apr 1
474 days
D
2006-57 FP
[32690]
2008 Mar 17
459 days
D
2006-57 FQ
2006-57 FR
[32691]
[32692]
2008 Mar 13
455 days
D
2014 - Version 1-13
(Compiled 2006)
Date of
orbital
Determination
Orbital
Inclination
(deg)
2008
2008
2008
2008
2008
2008
2008
2008
2008
2008
2008
2008
2008
2008
2008
2008
2008
2008
2008
2008
2008
2008
2008
2008
2008
2008
2008
2008
2008
2008
2008
2008
2008
2008
2008
2008
2008
2008
2008
2008
2008
2008
2008
2008
2008
2008
2008
2008
2008
2008
2008
59.39
57.71
57.69
57.69
58.29
58.27
59.70
59.71
58.71
58.69
58.99
58.94
58.64
58.22
58.19
57.73
58.28
58.26
58.63
57.80
58.02
58.02
56.46
56.45
58.77
58.40
58.51
58.69
58.64
58.78
58.17
58.14
57.97
57.72
58.44
58.42
56.61
56.61
58.41
59.93
59.93
57.63
58.67
58.66
58.87
58.86
56.04
56.04
58.61
58.28
58.27
Mar
Mar
Mar
Mar
Mar
Mar
Mar
Mar
Mar
Mar
Mar
Apr
Mar
Mar
Mar
Mar
Mar
Apr
Mar
Mar
Mar
Apr
Mar
Apr
Mar
Mar
Mar
Mar
Mar
Mar
Mar
Mar
Mar
Mar
Mar
Apr
Mar
Mar
Mar
Mar
Mar
Mar
Mar
Mar
Mar
Mar
Mar
Mar
Mar
Mar
Mar
8.93
5.17
14.60
5.18
5.17
10.06
5.12
5.94
5.80
10.96
6.91
5.74
5.92
6.91
11.04
6.70
6.91
2.72
6.87
6.10
6.90
8.52
7.90
3.56
7.89
6.55
7.93
7.70
21.64
7.90
7.82
13.70
7.84
7.74
7.94
2.77
7.83
19.67
7.82
7.84
14.06
7.83
10.63
14.99
10.82
30.47
9.90
14.02
9.72
10.79
11.97
Nodal
period
(min)
Extra Page 2006 -25
Semi
major axis
(km)
89.02
93.20
89.02
94.53
91.03
88.22
90.27
89.50
91.60
88.55
99.13
90.22
98.60
89.40
87.95
90.78
89.97
87.58
90.37
90.13
92.45
88.42
96.03
89.25
93.18
88.07
90.47
89.38
87.22
89.38
91.00
88.12
96.37
94.85
94.37
89.32
94.32
90.57
93.63
92.52
90.02
93.08
88.78
87.70
89.73
88.23
90.62
88.52
98.50
89.40
88.43
6605
6810
6605
6875
6704
6565
6666
6629
6732
6581
7096
6664
7070
6623
6552
6691
6651
6533
6671
6659
6773
6575
6947
6616
6809
6557
6676
6622
6515
6623
6702
6560
6963
6890
6866
6619
6864
6861
6831
6777
6654
6804
6593
6539
6640
6566
6684
6580
7086
6623
6576
Perigee
height
(km)
Apogee
height
(km)
Orbital
eccentric.
Argument
of perigee
(deg)
193
236
182
242
230
175
193
183
228
183
237
196
238
217
166
222
236
149
234
216
240
162
238
191
200
161
228
227
125
222
222
167
225
228
234
188
231
206
231
229
212
235
210
156
232
178
223
175
225
196
170
259
627
270
749
421
197
381
317
478
223
1198
375
1146
272
180
403
309
150
351
346
549
230
898
283
660
196
367
261
148
266
426
196
944
794
741
293
740
398
673
567
338
616
219
165
290
196
387
228
1150
293
224
0.005
0.028
0.007
0.037
0.014
0.002
0.014
0.010
0.019
0.003
0.068
0.013
0.064
0.004
0.001
0.014
0.006
0.0008
0.009
0.010
0.023
0.005
0.048
0.007
0.034
0.003
0.010
0.003
0.002
0.003
0.015
0.002
0.052
0.041
0.037
0.008
0.037
0.014
0.032
0.025
0.009
0.028
0.0007
0.0006
0.004
0.001
0.012
0.004
0.065
0.007
0.004
36
45
54
46
42
104
73
79
52
62
35
66
48
26
21
23
35
52
60
37
46
58
55
122
80
356
16
75
140
88
34
54
33
45
59
84
65
89
62
49
56
66
56
357
43
46
65
64
33
24
16
RAE Table of Earth Satellites
Year of Launch 2006
Cospar ID
[Norad number]
Descent date
Lifetime
D
2006-57 FS
[32693]
2008 Mar 14
456 days
D
2006-57 FT
[32694]
2008 Mar 17
459 days
D
2006-57 FU
2006-57 FV
[32695]
[32696]
2008 Apr 5
478 days
FW
FX
FY
FZ
GA
GB
[32697]
[32698]
[32700]
[32701]
[32702]
[32703]
2008 Mar 11
453 days
D
2006-57
2006-57
2006-57
2006-57
2006-57
2006-57
2008 Mar 17
459 days
D
2006-57 GC
[32704]
2008 Mar 17
459 days
D
2006-57 GD
[32714]
2008 Mar 23
465 days
2006-57
2006-57
2006-57
2006-57
[32731]
[32749]
[32755]
[35425]
D
GE
GF
GG
GH
2014 - Version 1-13
(Compiled 2006)
Date of
orbital
Determination
Orbital
Inclination
(deg)
2008
2008
2008
2008
2008
2008
2008
2008
2008
2008
2008
2008
2008
2008
2008
2008
2008
2008
2008
2008
2008
58.60
58.60
58.60
58.60
58.87
57.48
57.50
57.71
58.08
58.24
57.68
58.32
58.70
58.70
60.49
60.49
58.68
58.65
58.43
58.32
58.80
Mar
Mar
Mar
Mar
Mar
Mar
Apr
Mar
Mar
Mar
Mar
Mar
Mar
Mar
Mar
Mar
Mar
Mar
Mar
Mar
Mar
10.79
13.00
9.97
13.21
9.97
10.70
5.69
9.94
10.31
10.71
10.97
11.97
12.20
13.62
11.99
13.97
17.99
23.84
24.77
23.79
26.72
Nodal
period
(min)
Extra Page 2006 -26
Semi
major axis
(km)
88.72
87.73
89.93
89.40
103.07
104.02
88.63
104.52
112.53
97.93
88.82
93.23
88.93
88.15
92.23
90.77
94.90
89.20
88.97
89.42
93.93
6589
6541
6650
6623
7282
7327
6586
7351
7722
7038
6594
6812
6600
6562
6763
6691
6892
6614
6602
6624
6846
Perigee
height
(km)
Apogee
height
(km)
Orbital
eccentric.
Argument
of perigee
(deg)
198
158
220
208
237
234
161
236
212
232
185
208
183
162
220
206
217
181
201
205
224
223
166
322
280
1570
1663
253
1707
2474
1087
246
658
260
204
548
418
810
289
245
286
711
0.002
0.0006
0.008
0.005
0.092
0.098
0.007
0.100
0.147
0.061
0.005
0.033
0.006
0.003
0.024
0.016
0.043
0.008
0.003
0.006
0.036
3
351
31
38
45
42
43
47
31
55
40
42
110
113
37
39
67
84
46
72
68