RAE Table of Earth Satellites
Year of Launch 1992
Name
[Launcher]
Fragments
Cospar ID
[Norad #] Launchsite
Cospar ID
(Revised 2001)
Launchdate
Lifetime + Descent date
[Norad]
Shape and
weight (kg)
Descent date
Size
(m)
Lifetime
Date of
orbital
determination
Orbital
Inclination
(deg)
Nodal
period
(min)
Semi
major axis
(km)
Page 1081
Perigee
height
(km)
Apogee
height
(km)
Orbital
Argument
eccentricity of perigee
(deg)
D
R
Cosmos 2175
[Soyuz 11A511U]
1992-01 A
(21844)
PLE
1992 Jan 21.63
59.2 days
1992 Mar 20.8
Spherecylinder
6600
7 long?
2.4 dia
1992 Jan 26.2
67.14
89.74
6639
184
337
0.011
73
D
Cosmos 2175
Block I 3rd stage
1992-01 B
(21845)
1992 Jan 21.63
3 days
1992 Jan 24
Cylinder
2500?
7.5 long
2.6 dia
1992 Jan 21.9
67.13
89.50
6627
164
335
0.013
97
D STS 42*
7M (Discovery F14)
R [Shuttle]
1992-02 A
(21846)
CC-LC39A
1992 Jan 22.62
8.05 days
1992 Jan 30.67
Cylinder +
delta wing
98543 empty
37.1 long
17.4 high
23.8 span
1992 Jan 23.1
56.97
90.49
6678
294
306
0.001
261
Cosmos 2176
[Molniya
8K78M / 2 BL]
1992-03 A
(21847)
PLE-LC43/4
1992 Jan 24.05
100 years?
Windmill +
6 vanes
1250?
4.2 long?
1.6 dia
1992 Jan 24.1
1992 Feb 15.0
2001 Dec 19.19
62.78
62.80
66.08
709.02
717.80
718.33
26339
26556
26569
573
626
3317
39350
39730
37065
0.736
0.736
0.635
319
320
267
D
Cosmos 2176
Block I 3rd stage
1992-03 B
(21848)
1992 Jan 24.05
26 days
1992 Feb 19
Cylinder
2500?
7.5 long
2.6 dia
1992 Jan 26.7
62.75
92.49
6775
210
583
0.028
118
D
Cosmos 2176
4th stage casing
1992-03 C
(21849)
1992 Jan 24.05
12 days
1992 Feb 5
Irregular
1992 Jan 24.5
62.82
92.56
6778
175
625
0.033
121
Cosmos 2176
Block L 4th stage
1992-03 D
(21850)
1992 Jan 24.05
100 years?
Cylinder
440 empty
2.0 long
2.0 dia
1992 Jan 26.1
2001 Dec 12.23
62.74
66.71
706.18
706.13
26269
26268
606
1879
39175
37899
0.734
0.686
319
239
D
Progress-M 11**
[Soyuz 11A511U2
R15000-058]
1992-04 A
(21851)
BAI-LC1
1992 Jan 25.33
48.33 days
1992 Mar 13.66
Spherecylinder +
2 panels
7020?
7.9 long?
2.3 dia?
1992 Jan 25.8
51.60
90.13
6662
264
304
0.003
301
D
Progress-M 11
1992-04 B
Block I 3rd stage (21852)
1992 Jan 25.33
1 day
1992 Jan 26
Cylinder
2500?
7.5 long?
2.6 dia?
1992 Jan 25.4
51.62
88.49
6581
186
220
0.003
105
*
-
Launched from Cape Canaveral (1 Canadian woman payload specialist, 6 men including a German ESA payload specialist);
landed at Edwards AFB, California. Cargo bay carried International Microgravity Laboratory, IML-1 (not separated).
** Progress-M 11 docked with Mir (+X port) on 1992 Jan 27.40. Undocked 1992 Mar 13.36 and de-orbited.
2004 December 31 – version 1.01
RAE Table of Earth Satellites
Year of Launch 1992
Name
[Launcher]
Fragments
Launchdate
Lifetime + Descent date
[Norad]
Shape and
weight (kg)
Descent date
Cosmos 2177
1992-05 A
(Glonass 53)
(21853)
[Proton 8K82K
BAI-LC81L
372-02/11S861 59L]
1992 Jan 29.93
1 million
years
Cylinder +
panels +
boom 1400
L
Cosmos 2178
(Glonass 54)
[Proton]
1992-05 B
(21854)
1992 Jan 29.93
1 million
years
L
Cosmos 2179
(Glonass 55)
[Proton]
1992-05 C
(21855)
D
Cosmos 2177
third stage
D
Orbital
Inclination
(deg)
Nodal
period
(min)
-
1992 Feb 6.0
1992 Feb 20.2
2001 Dec 19.49
64.78
64.81
65.91
Cylinder +
panels +
boom 1400
-
1992 Feb 6.0
1992 Feb 17.2
2001 Dec 21.15
1992 Jan 29.93
1 million
years
Cylinder +
panels +
boom 1400
-
1992-05 D
(21856)
1992 Jan 29.93
1 day
1992 Jan 30
Cylinder
Cosmos 2177
4th stage casing
1992-05 E
[21857]
1992 Jan 29.93
1 day
1992 Jan 30
Cosmos 2177
Block DM
fourth stage
1992-05 F
(21858)
1992 Jan 29.93
1 million
years
D
Cosmos 2177
Ullage motor
1992-05 G
[21862]
D
Cosmos 2177
Ullage motor
1992-05 H
[21862]
1992
2155
1997
1992
2060
1997
DSCS 3B-01
(USA 78)
[Atlas 2 AC-101
Centaur II 8101]
1992-06 A
(21873)
CC-LC36A
Atlas 2
Centaur 101 stage
IABS-01**
D
Page 1082
Semi
major axis
(km)
Perigee
height
(km)
Apogee
height
(km)
Orbital
Argument
eccentricity of perigee
(deg)
684.42
675.74
675.73
25726
25508
25508
19135
19112
19107
19561
19148
19152
0.008
0.001
0.0009
98
194
220
64.79
64.79
65.92
668.24
675.74
675.72
25319
25508
25508
18752
19088
19088
19130
19172
19170
0.007
0.002
0.002
89
11
12
1992 Feb 5.5
1992 Feb 15.8
2001 Dec 20.32
64.79
64.79
65.92
675.20
675.74
675.73
25494
25508
25508
19090
19111
19114
19142
19149
19144
0.001
0.001
0.0006
234
207
228
6.5 long?
4 dia
1992 Jan 30.3
64.84
87.32
6519
137
145
0.001
252
Cylinder
17300 full
5.5 long
4.0 dia
1992 Feb 1.3
2001 Dec 21.20
64.79
65.91
675.38
675.37
25499
25499
19110
19108
19132
19133
0.0004
0.0005
246
95
Ellipsoid
55
1.0 long
0.6 dia
Ellipsoid
55
1.0 long
0.6 dia
1992 Feb 11.03
>million
years?
Box +
2 vanes?
1150 full?
875 empty?
2 long?
2.7 dia?
No elements available
1992-06 B
(21874)
1992 Feb 11.03
2319 days
1998 Jun 18
Cylinder
2000?
10.1 long
3.05 dia
1992 Feb 11
1998 Jun 17.49
0.731
0.004
- *
134
1992-06 C
(21877)
1992 Feb 11.03
>million
years
-
-
* Based on a trade press report.
** Integrated Apogee Boost System.
2004 December 31 – version 1.01
Jan 29.93
days
Dec 23
Jan 29.93
days
Oct 20
Size
(m)
Lifetime
(Revised 2001)
Date of
orbital
determination
L
Cospar ID
[Norad #] Launchsite
Cospar ID
Orbital data not released
25.87
628.2
87.47
24312
6528
173
122
35695
177
Orbital data not released
No elements available
A spin-stabilised propulsion stage, reported to have separated in geosynchronous orbit.
RAE Table of Earth Satellites
Year of Launch 1992
Name
[Launcher]
Fragments
Cospar ID
[Norad #] Launchsite
Cospar ID
(Revised 2001)
Launchdate
Lifetime + Descent date
[Norad]
Shape and
weight (kg)
Descent date
Size
(m)
Lifetime
Date of
orbital
determination
Orbital
Inclination
(deg)
Nodal
period
(min)
Semi
major axis
(km)
Page 1083
Perigee
height
(km)
Apogee
height
(km)
Orbital
Argument
eccentricity of perigee
(deg)
D
Fuyo 1*
(JERS 1)
[H-1 H24(F)]
1992-07 A
(21867)
TAN-LCO
1992 Feb 11.08
3583 days
2001 Dec 3
Box +
paddle
+ plate
1340
0.93 x
1.83 x
3.16
1992 Feb 16.7
2001 Dec 3
97.69
97.59
96.14
87.40
6949
6525
567
138
574
154
0.001
0.001
186
295
D
H-1 second
stage
1992-07 B
(21868)
1992 Feb 11.08
848 days
1995 Feb 28
Cylinder
10800 full
2000 empty
10.32 long
2.49 dia
1992 Feb 16.6
97.70
94.73
6881
445
560
0.008
186
Cosmos 2180
[Cosmos 11L65M
65078-418]
1992-08 A
(21875)
PLE
1992 Feb 17.92
1200 years
Cylinder
810
2.1 long
2.0 dia
1992 Feb 19.7
2001 Dec 19.58
82.93
82.93
104.94
104.85
7367
7366
962
958
1016
1016
0.004
0.004
282
22
Cosmos 2180
2nd stage
1992-08 B
(21876)
1992 Feb 17.92
600 years
Cylinder
2200?
7.4 long
2.4 dia
1992 Feb 19.7
2001 Dec 21.12
82.93
82.93
104.83
104.72
7362
7360
962
955
1005
1007
0.003
0.003
278
343
GPS 2-12 (USA 79)
(Navstar 25)
[Delta 7925 #207]
1992-09 A
(21890)
CC-LC17B
1992 Feb 23.94
1 million
years
Cylinder +
4 vanes
1667 full
844 empty
5.3 span?
2.4 long?
1.8 dia?
1992 Feb 25.8
1992 Mar 15.6
2001 Dec 19.46
54.98
54.71
53.77
715.02
717.89
717.92
26488
26559
26559
19901
20018
19928
20319
20343
20433
0.008
0.006
0.010
153
137
251
Delta 2
second stage
1992-09 B
(21891)
1992 Feb 23.94
30 years
Cylinder
6983 full
919 empty
5.88 long
2.44 dia
1992 Feb 25.4
2001 Dec 20.06
20.00
20.00
98.02
97.73
7053
7029
628
610
721
690
0.007
0.006
185
208
GPS 2-12
PAM-D PKM
1992-09 C
(21892)
1992 Feb 23.94
2240 days
1998 Apr 12
Cylinder
2154?
full
2.29 long
1.5 dia
1992 Feb 26.8
1998 Apr 12.17
34.67
34.39
355.74
88.82
16639
6595
186
125
20335
307
0.605
0.014
195
86
GPS 2-12 fragment
1992-09 D
[26792]
2001 Nov 18.03
34.39
258.58
13445
255
13878
0.507
243
D
*
Japanese Earth Resources Satellite.
2004 December 31 – version 1.01
Fuyo means Rose Mallow.
RAE Table of Earth Satellites
Year of Launch 1992
Name
[Launcher]
Fragments
Cospar ID
[Norad #] Launchsite
Cospar ID
(Revised 2001)
Launchdate
Lifetime + Descent date
[Norad]
Shape and
weight (kg)
Descent date
Size
(m)
Lifetime
Date of
orbital
determination
Orbital
Inclination
(deg)
Page 1084
Nodal
period
(min)
Semi
major axis
(km)
Perigee
height
(km)
Apogee
height
(km)
Orbital
Argument
eccentricity of perigee
(deg)
Superbird B1*
[Ariane 4-21]
1992-10 A
(21893)
KOU-ELA2
1992 Feb 27.00†
>million
years
Box +
panels
1532 full
1224 empty
3.4 x
2.41 x
2.20
20.3 span
1992
1992
1992
1992
2001
Feb
Feb
Mar
Mar
Dec
28.1
29.2
3.1
15.1
21.59
3.68
0.10
0.07
0.10
0.39
744.15
1355.08
1433.77
1436.03
1453.77
27209
40566
42121
42165
42510
5855
32547
35653
35767
36048
35806
35829
35834
35807
36215
0.550
0.040
0.002
0.0005
0.002
178
46
68
258
227
Arabsat 1C**
[Ariane 4-21]
1992-10 B
(21894)
1992 Feb 27.00†
>million
years
Box +
panels
785 full
600 empty
2.26 x
1.64 x
1.49
20.7 span
1992
1992
1992
1992
2001
Feb
Feb
Mar
Mar
Dec
28.8
29.5
1.5
20.4
20.60
1.56
0.14
0.01
0.07
0.08
991.87
1373.70
1419.05
1436.00
1436.07
32949
40936
41832
42165
42164
17339
33306
35056
35776
35759
35802
35811
35853
35797
35812
0.280
0.031
0.010
0.0002
0.0006
182
179
175
357
119
Ariane 44L V49
3rd stage [H10]
1992-10 C
(21895)
1992 Feb 27.00†
2268 days
1998 May 14
Cylinder
11762 full
1262 empty
9.9 long
2.6 dia
1992 Feb 27.2
7.02
630.76
24379
218
35784
0.729
178
Molniya-1 83
[Molniya
8K78M / ML
1992-11 A
(21897)
PLE
1992 Mar 4.18
10 years?
Windmill +
6 vanes
1000?
3.4 long
1.6 dia
1992 Mar 9.1
1992 Mar 17.1
2001 Dec 21.61
62.93
62.81
64.90
702.58
717.69
718.02
26179
26553
26562
610
620
1014
38993
39731
39352
0.733
0.736
0.722
288
288
252
D
Molniya-1 83
Block I 3rd stage
1992-11 B
(21898)
1992 Mar 4.18
24 days
1992 Mar 28
Cylinder
2500?
7.5 long
2.6 dia
1992 Mar 4.7
62.80
92.08
6755
219
535
0.023
123
D
Molniya-1 83
4th stage casing
1992-11 C
(21899)
1992 Mar 4.18
15 days
1992 Mar 19
Irregular
-
1992 Mar 5.4
62.82
92.33
6767
185
593
0.030
118
Molniya-1 83
Block DM
4th stage
1992-11 D
(21900)
1992 Mar 4.18
14.5 years
Cylinder
440
empty
2.0 long
2.0 dia
1992 Mar 7.6
2001 Dec 19.61
62.84
64.62
698.44
698.40
26077
26076
607
699
38790
38694
0.732
0.729
288
250
Cosmos 2181
[Cosmos 11K65M
53778-423]
1992-12 A
(21902)
PLE
1992 Mar 9.95
1200 years
Cylinder
810
2.1 long
2.0 dia
1992 Mar 18.0
2001 Dec 20.26
82.95
82.94
105.03
104.95
7371
7370
973
969
1013
1014
0.003
0.003
249
78
Cosmos 2181
2nd stage
1992-12 B
(21903)
1992 Mar 9.95
600 years
Cylinder
2200?
7.4 long
2.4 dia
1992 Mar 14.9
2001 Dec 21.24
82.94
82.94
104.85
104.80
7363
7364
966
952
1004
1018
0.003
0.004
236
12
D
* Domestic communications satellite for Space Communications Corporation, Japan.
** Arab Satellite Communications Organisation satellite.
† Launch at 2358 UT, 1992 Feb 26.
2004 December 31 – version 1.01
RAE Table of Earth Satellites
Year of Launch 1992
Name
[Launcher]
Fragments
Cospar ID
[Norad #] Launchsite
Cospar ID
(Revised 2001)
Launchdate
Lifetime + Descent date
[Norad]
Shape and
weight (kg)
Descent date
Size
(m)
Lifetime
Date of
orbital
determination
Orbital
Inclination
(deg)
Galaxy 5*
1992-13 A
[Atlas 1 MPF AC-72 (21906)
Centaur I 5052]
CC-LC36B
1992 Mar 14.00
>million
years
Cylinder +
skirt
788 full
2.82 to
6.7 long
2.16 dia
1992
1992
1992
1992
2001
16.5
17.9
18.8
24.9
20.13
Centaur 72
stage
1992-13 B
(21907)
1992 Mar 14.00
1 million
years
Cylinder
18515 full
4725 empty
9.15 long
3.05 dia
D Soyuz-TM 14**
3M [Soyuz 11A511U2]
R
1992-14 A
(21908)
BAI-LC1
1992 Mar 17.45
145.60 days
1992 Aug 10.5
Spherecylinder +
2 panels
7070
D
1992-14 B
(21909)
1992 Mar 17.45
2 days
1992 Mar 19
1992-15 A
(21915)
CC-LC39A
Soyuz-TM 14
Block I 3rd stage
D STS 45***
7M (Atlantis F11)
R [Shuttle]
D
R
Cosmos 2182
[Soyuz 11A511U]
D
Cosmos 2182
Block I 3rd stage
Page 1085
Nodal
period
(min)
Semi
major axis
(km)
Perigee
height
(km)
Apogee
height
(km)
Orbital
Argument
eccentricity of perigee
(deg)
19.69
0.35
0.21
0.14
0.04
655.35
1407.51
1414.24
1436.06
1436.07
25004
41605
41738
42166
42164
1120
34564
34810
35695
35781
36132
35891
35909
35881
35791
0.700
0.016
0.013
0.002
0.0001
180
195
201
137
118
1992 Mar 16.0
2001 Dec 19.93
19.71
19.21
637.89
638.30
24558
24557
1107
1139
35254
35218
0.695
0.694
181
97
7.5 long
2.3 to
2.72 dia
1992 Mar 17.8
51.60
90.11
6661
263
303
0.003
145
Cylinder
2500?
7.5 long
2.6 dia
1992 Mar 17.5
51.65
88.72
6592
192
236
0.003
100
1992 Mar 24.55
8.92 days
1992 Apr 2.47
Cylinder +
delta wing
93007
empty
37.1 long
17.4 high
23.8 span
1992 Mar 24.6
1992 Mar 24.8
57.01
57.00
90.28
90.42
6668
6675
278
292
302
302
0.002
0.001
270
280
1992-16 A
(21920)
PLE
1992 Apr 1.60
59.2 days
1992 May 30.8
Spherecylinder
6700?
7 long?
2.4 dia
1992 Apr 3.0
67.16
89.33
6619
166
315
0.011
93
1992-16 B
(21921)
1992 Apr 1.60
3 days
1992 Apr 4
Cylinder
2500?
7.5 long
2.6 dia
1992 Apr 1.9
67.15
89.29
6617
162
315
0.012
95
Mar
Mar
Mar
Mar
Dec
* Hughes Communications Inc.
** Soyuz-TM 14 docked with Kvant-1 (-X port) on 1992 Mar 19.52, with 2 CIS and 1 German cosmonaut, the Mir '92 mission.
Undocked 1992 Aug 9.91 and landed 136 km E of Dzhezkazgan with its commander and flight engineer and the French
cosmonaut (see page 1096).
*** Launch and landing at Cape Canaveral (1 woman, 6 men including a Belgian ESA payload specialist). Cargo bay carried
Atmospheric Laboratory for Applications and Science, ATLAS-1 (not separated).
2004 December 31 – version 1.01
RAE Table of Earth Satellites
Year of Launch 1992
Name
[Launcher]
Fragments
Shape and
weight (kg)
Descent date
Gorizont 25*
1992-17 A
[Proton 8K82K
(21922)
369-01/11S861 57L] BAI-LC81L
1992 Apr 2.08
>million
years
Cylinder +
dish +
panels
2125
D
Gorizont 25
third stage
1992-17 B
(21923)
1992 Apr 2.08
2 days
1992 Apr 4
Cylinder
6.5 long?
4 dia
1992 Apr 2.4
51.64
D
Gorizont 25
4th stage casing
1992-17 C
(21924)
1992 Apr 2.08
<1 day
1992 Apr 2
Irregular
-
1992 Apr 2.4
51.64
Gorizont 25
Block DM-2
fourth stage
1992-17 D
(21925)
1992 Apr 2.08
>million
years
Cylinder
17300 full
5.5 long
4.0 dia
1992 Apr 10.9
2001 Dec 20.64
1.46
5.73
D
Gorizont 25
Ullage motor
1992-17 E
[21926]
1992 Apr 2.08
191 days
1992 Oct 23
Ellipsoid
55
1.0 long
0.6 dia
D
Gorizont 25
Ullage motor
1992-17 F
[21927]
1992 Apr 2.08
203 days
1992 Nov 4
Ellipsoid
55
1.0 long
0.6 dia
D
Cosmos 2183
[Soyuz 11A511U]
1992-18 A
(21928)
BAI
1992 Apr 8.52
297.0 days
1993 Feb 16.5
Spherecylinder
6600
7 long?
2.4 dia
1992 Apr 9.4
64.87
D
Cosmos 2183
Block I 3rd stage
1992-18 B
(21929)
1992 Apr 8.52
2 days
1992 Apr 10
Cylinder
2500?
7.5 long
2.6 dia
1992 Apr 8.8
GPS 2-13 (USA 80)
(Navstar 26)
[Delta 7925 #208]
1992-19 A
(21930)
CC-LC17B
1992 Apr 10.14
1 million
years
Cylinder +
4 vanes
1667 full
844 empty
5.3 span?
2.4 long?
1.8 dia?
Delta 2
second stage
1992-19 B
(21931)
1992 Apr 10.14
20 years
Cylinder
6983 full
919 empty
5.88 long
2.44 dia
Ministry of Communications of the Russian Federation.
2004 December 31 – version 1.01
Size
(m)
Lifetime
(Revised 2001)
Launchdate
Lifetime + Descent date
[Norad]
*
Cospar ID
[Norad #] Launchsite
Cospar ID
-
Date of
orbital
determination
Orbital
Inclination
(deg)
1992
1992
1992
2001
1.46
1.44
1.34
5.78
Page 1086
Nodal
period
(min)
Semi
major axis
(km)
Perigee
height
(km)
Apogee
height
(km)
Orbital
Argument
eccentricity of perigee
(deg)
1428.20
1435.80
1436.04
1436.03
42012
42161
42166
42164
35580
35769
35767
35778
35689
35796
35808
35792
0.001
0.0003
0.0005
0.0002
234
230
216
268
88.22
6568
187
192
0.0004
314
88.22
6567
178
201
0.002
27
41937
41936
35463
35454
35653
35661
0.002
0.002
281
188
89.85
6645
240
294
0.004
84
64.87
88.89
6597
186
252
0.005
63
1992 Apr 12.8
1992 Apr 19.7
2001 Dec 21.08
55.18
55.12
54.61
715.78
717.94
717.85
26507
26560
26557
19871
19979
20099
20387
20385
20258
0.010
0.008
0.003
157
158
19
1992 Apr 12.1
2001 Dec 19.62
21.18
21.17
96.95
95.87
7001
6939
531
496
716
625
0.013
0.009
199
108
Apr
Apr
May
Dec
5.0
11.9
19.8
20.65
1424.35
1424.43
1992-19 continued on page 1087
RAE Table of Earth Satellites
Year of Launch 1992
Name
[Launcher]
Fragments
D
Cospar ID
[Norad #] Launchsite
Cospar ID
(Revised 2001)
Launchdate
Lifetime + Descent date
[Norad]
Shape and
weight (kg)
Descent date
Size
(m)
Lifetime
Date of
orbital
determination
Orbital
Inclination
(deg)
Nodal
period
(min)
Cylinder
2154?
full
2.29 long
1.5 dia
1992 Apr 13.2
1998 Aug 16.41
34.61
34.29
357.17
88.27
2002 Feb 3.21
34.74
Semi
major axis
(km)
Page 1087
Perigee
height
(km)
Apogee
height
(km)
Orbital
Argument
eccentricity of perigee
(deg)
16683
6567
190
125
20420
251
0.606
0.010
196
174
249.75
13138
216
13302
0.498
248
GPS 2-13
PAM-D PKM
1992-19 C
(21932)
1992 Apr 10.14
2319 days
1998 Aug 16
GPS 2-13 fragment
1992-19 D
[26791]
Cosmos 2184
[Cosmos 11K65M
47178-419]
1992-20 A
(21937)
PLE
1992 Apr 15.30
1200 years
Cylinder
810
2.1 long
2.0 dia
1992 Apr 17.5
2001 Dec 21.75
82.94
82.93
104.98
104.88
7369
7368
967
964
1014
1014
0.003
0.003
274
172
Cosmos 2184
2nd stage
1992-20 B
(21938)
1992 Apr 15.30
600 years
Cylinder
2200?
7.4 long
2.4 dia
1992 Apr 16.1
2001 Dec 21.19
82.93
82.93
104.85
104.73
7366
7361
965
959
1004
1004
0.003
0.003
269
128
Telecom 2B*
[Ariane 4-22]
1992-21 A
(21939)
KOU-ELA2
1992 Apr 15.98
>million
years
Box +
panels
1380 full
1124 empty
3.1 x
2.6 x
1.9
22 span
1992
1992
1992
2001
Apr
May
Jun
Dec
18.4
13.4
4.3
18.86
1.50
0.34
0.07
0.92
761.36
1425.42
1436.02
1436.05
27626
41958
42165
42164
6717
35385
35777
35768
35779
35774
35797
35803
0.526
0.005
0.0002
0.0004
179
26
136
157
Inmarsat 2 F-4
[Ariane 4-22]
1992-21 B
(21940)
1992 Apr 15.98
>million
years
Box +
panels
824 full
624 empty
2.4 x
1.6 x
1.5
14.9 span
1992
1992
1992
2001
Apr
Apr
May
Dec
19.8
20.6
13.5
20.19
2.31
2.00
2.07
2.45
1041.75
1430.61
1435.97
1436.17
34044
42059
42164
42166
19546
35558
35773
35778
35786
35804
35799
35797
0.239
0.003
0.0003
0.0002
177
175
153
237
Ariane 44L V50
3rd stage[H 10+]**
1992-21 C
(21941)
1992 Apr 15.98
disintegrated
1993 Apr 21
Cylinder
12072 full
1232 empty
11.7 long
2.6 dia
1992 Apr 16.7
2001 Dec 20.55
3.95
3.88
641.58
446.48
24657
19351
336
201
36222
25744
0.728
0.660
179
351
Ariane 44L V50
Spelda top
1992-21 D
[21942]
1992 Apr 15.98
2001 Dec 20.07
3.57
507.19
21071
337
29048
0.681
178
Fragments
1992-21 E-R
12 pieces
For orbital information see extra pages at the end of the year
D
Progress-M 12†
[Soyuz 11A511U2
R15000-059]
1992-22 A
(21946)
BAI-LC1
1992 Apr 19.90
69.10 days
1992 Jun 28.00
Spherecylinder +
2 panels
7020?
7.9 long?
2.3 dia?
1992 Apr 20.6
51.60
90.46
6678
279
321
0.003
100
D
Progress-M 12
Block I 3rd stage
1992-22 B
(21947)
1992 Apr 19.90
2 days
1992 Apr 21
Cylinder
2500?
7.5 long?
2.6 dia?
1992 Apr 20.6
51.66
87.83
6549
167
174
0.001
78
* French domestic communications satellite incorporating Syracuse 2 X-band military payload.
** First use of H10+ third stage.
† Progress-M 12 docked with Mir (+X port) on 1992 Apr 21.98. Undocked 1992 Jun 27.90 and de-orbited late on Jun 27.
2004 December 31 – version 1.01
RAE Table of Earth Satellites
Year of Launch 1992
Name
[Launcher]
Fragments
Cospar ID
[Norad #] Launchsite
Cospar ID
Launchdate
Lifetime + Descent date
[Norad]
Shape and
weight (kg)
Descent date
Size
(m)
Lifetime
(Revised 2001)
Date of
orbital
determination
Orbital
Inclination
(deg)
Nodal
period
(min)
1992 May 21.0
2001 Dec 20.76
85.14
85.02
100.82
100.67
Semi
major axis
(km)
Apogee
height
(km)
Orbital
Argument
eccentricity of perigee
(deg)
784
788
805
793
0.002
0.0002
USA 81(SBWASS R3)
[Titan 2 SLV
23G-3]
1992-23 A
(21949)
VDB-SLC4W
1992 Apr 25.37
300 years
-
-
Titan 2
2nd stage
1992-23 B
(21950)
1992 Apr 25.37
?
?
-
-
D
R
Resurs-F 14
[Soyuz 11A511U]
1992-24 A
(21951)
PLE-LC43/4
1992 Apr 29.38
29.7 days
1992 May 29.1
Sphere-cone
+ panels
6300
6.5 long?
2.4 dia
1992 Apr 30.0
82.09
89.22
6611
231
235
0.0003
286
D
Resurs-F 14
Block I 3rd stage
1992-24 B
(21952)
1992 Apr 29.38
2 days
1992 May 1
Cylinder
2500?
7.5 long
2.6 dia
1992 Apr 29.8
82.08
88.58
6579
179
224
0.003
83
D
Resurs-F 14
engine
1992-24 C
(21975)
1992 Apr 29.38
31 days
1992 May 30
Cone
600?
full
1.9 long
1.0 dia
1992 May 30.5
82.07
87.89
6545
156
178
0.002
259
D
R
Cosmos 2185
[Soyuz 11A511U]
1992-25 A
(21953)
BAI
1992 Apr 29.42
43.5 days
1992 Jun 11.9
Spherecylinder
6700?
7 long?
2.4 dia
1992 Apr 30.2
69.97
89.43
6623
211
279
0.005
8
D
Cosmos 2185
Block I 3rd stage
1992-25 B
(21954)
1992 Apr 29.42
4 days
1992 May 3
Cylinder
2500?
7.5 long
2.6 dia
1992 Apr 30.1
69.98
89.22
6613
193
276
0.006
70
*
Orbital data based on visual observations by amateur observers.
D
2004 December 31 – version 1.01
7173
7169
Page 1088
Perigee
height
(km)
73*
95
Orbital data not released
No elements available
RAE Table of Earth Satellites
Year of Launch 1992
Name
[Launcher]
Fragments
Cospar ID
[Norad #] Launchsite
Cospar ID
(Revised 2001)
Launchdate
Lifetime + Descent date
[Norad]
Shape and
weight (kg)
Descent date
Size
(m)
Lifetime
Date of
orbital
determination
Orbital
Inclination
(deg)
1992-26 A
(21963)
CC-LC39B
1992 May 7.99
8.88 days
1992 May 16.87
Cylinder +
delta wing
91212
empty
37.1 long
17.4 high
23.8 span
1992
1992
1992
1992
28.33
28.31
28.31
28.31
Intelsat 6-3
Orbus 215 PKM
1990-21 A*
[20523]
1992 May 7.99
1 million
years?
Spherecone
10400 full
640 empty
3.15 long
2.34 dia
1992 May 15
2004 Dec 30.98
28.3
2.24
Palapa 7**
(Flight B-4)
[Delta 7925 #209]
1992-27 A
(21964)
CC-LC17B
1992 May 14.03
>million
years
Cylinder
1200? full
650? empty
2.82 to
6.32 long
2.6 dia
1992
1992
1992
2001
19.1
20.0
17.9
18.67
Delta 2
second stage
1992-27 B
(21965)
1992 May 14.03
200 years
Cylinder
6983 full
919 empty
5.88 long
2.44 dia
Palapa 7
PAM-D PKM
1992-27 C
(21966)
1992 May 14.03
1 million
years
Cylinder
2154?
full
D
Fragment
1992-27 D
[23312]
D
SROSS-C***
[ASLV-D3]
1992-28 A
(21968)
SRI
D
ASLV-D3
fourth stage
1992-28 B
(21967)
D STS 49*
7M (Endeavour F1)
R [Shuttle]
*
Apogee
height
(km)
Orbital
Argument
eccentricity of perigee
(deg)
6686
6744
6741
6731
279
362
355
344
337
370
370
362
0.004
0.001
0.001
0.001
56
196
222
152
1535.7
1436.10
44111
42165
345
35773
75120
35800
0.848
0.0003
180†
226
0.39
0.15
0.16
0.006
1397.81
1414.40
1436.07
1436.17
41414
41741
42166
42166
34262
34924
35777
35784
35810
35802
35799
35792
0.019
0.011
0.0003
0.0001
193
169
176
43
1992 May 15.9
2001 Dec 20.25
19.70
19.68
119.02
118.75
8025
8003
502
501
2791
2747
0.143
0.140
204
231
2.29 long
1.5 dia
1992 May 19.0
2001 Dec 18.52
22.68
22.54
700.96
701.30
26147
26147
2808
2812
36730
36726
0.649
0.649
1
155
1996 Oct 22
1622 days
1994 Oct 7.50
19.70
114.24
7799
595
2247
0.106
238
1992 May 20.02
55.5 days
1992 Jul 14.5
Octagonal
prism
107
1.10 high
0.82 dia
1992 May 20.5
46.03
91.29
6721
251
434
0.014
317
1992 May 20.02
35 days
1992 Jun 24
Cylinder
186 empty
1.69 long
0.65 dia
1992 May 22.5
46.03
91.26
6719
254
428
0.013
328
May
May
Jun
Dec
8.5
11.2
14.0
14.2
90.48
91.67
91.60
91.40
Semi
major axis
(km)
Page 1089
Perigee
height
(km)
May
May
May
May
Nodal
period
(min)
Launched from Cape Canaveral (1 woman, 6 men); landed at Edwards AFB, California. Rendezvoused with Intelsat 6-3
(1990-21 A, page 1014) on 1992 May 10.85, May 11.85 and May 13.99, successfully capturing it on the third occasion; attached a new perigee kick motor
in Space Shuttle's cargo bay, then released into orbit again 4 hr 54 min later.
Cargo bay carried Assembly of Space Station by EVA Methods, ASEM (not separated).
** Satellite for PT Telekomunikasi Indonesia (Telkom).
*** Stretched Rohini Satellite Series. Indian aeronomy and gamma-ray burst satellite launched from Sriharikota by
Augmented Satellite Launch Vehicle. Failed to attain intended circular orbit.
† Estimated orbit - the perigee kick motor has yet to be catalogued.
2004 December 31 – version 1.01
RAE Table of Earth Satellites
Year of Launch 1992
Name
[Launcher]
Fragments
Cospar ID
[Norad #] Launchsite
Cospar ID
(Revised 2001)
Launchdate
Lifetime + Descent date
[Norad]
Shape and
weight (kg)
Descent date
Size
(m)
Lifetime
Date of
orbital
determination
Orbital
Inclination
(deg)
Nodal
period
(min)
1992-29 A
(21973)
PLE
1992 May 28.80
57.0 days
1992 Jul 24.8
Spherecylinder
6700?
7 long?
2.4 dia
1992 May 30.5
62.85
89.84
Semi
major axis
(km)
Page 1090
Perigee
height
(km)
Apogee
height
(km)
Orbital
Argument
eccentricity of perigee
(deg)
6645
182
352
0.013
73
D
R
Cosmos 2186
[Soyuz 11A511U]
D
Cosmos 2186
Block I 3rd stage
1992-29 B
(21974)
1992 May 28.80
6 days
1992 Jun 3
Cylinder
2500?
7.5 long
2.6 dia
1992 May 30.3
62.83
89.31
6619
182
299
0.009
119
Cosmos 2187 *
[Cosmos 11K65M
53742-114]
1992-30 A
(21976)
PLE
1992 Jun 3.04
10000 years
Spheroid
45
1.0 long?
0.8 dia?
1992 Jun 5.2
2001 Dec 20.26
74.01
74.00
114.73
114.68
7820
7819
1402
1401
1480
1481
0.005
0.005
107
223
Cosmos 2188 *
[Cosmos]
1992-30 B
(21977)
1992 Jun 3.04
10000 years
Spheroid
45
1.0 long?
0.8 dia?
1992 Jun 5.2
2001 Dec 19.76
74.00
74.00
114.56
114.52
7812
7812
1389
1387
1479
1479
0.006
0.006
97
197
Cosmos 2189 *
[Cosmos]
1992-30 C
(21978)
1992 Jun 3.04
10000 years
Spheroid
45
1.0 long?
0.8 dia?
1992 Jun 5.3
2001 Dec 19.89
74.00
74.00
114.89
114.83
7827
7826
1418
1415
1479
1480
0.004
0.004
105
239
Cosmos 2190 *
[Cosmos]
1992-30 D
(21979)
1992 Jun 3.04
10000 years
Spheroid
45
1.0 long?
0.8 dia?
1992 Jun 5.3
2001 Dec 21.14
74.00
74.00
115.05
115.00
7834
7834
1431
1430
1480
1480
0.003
0.003
111
259
Cosmos 2191 *
[Cosmos]
1992-30 E
(21980)
1992 Jun 3.04
10000 years
Spheroid
45
1.0 long?
0.8 dia?
1992 Jun 3.7
2001 Dec 21.41
74.01
74.00
115.76
115.70
7866
7866
1473
1473
1503
1501
0.002
0.002
220
83
Cosmos 2192 *
[Cosmos]
1992-30 F
(21981)
1992 Jun 3.04
10000 years
Spheroid
45
1.0 long?
0.8 dia?
1992 Jun 5.3
2001 Dec 19.98
74.00
74.00
115.56
115.50
7857
7857
1472
1472
1486
1485
0.001
0.0008
184
26
Cosmos 2193 *
[Cosmos]
1992-30 G
(21982)
1992 Jun 3.04
10000 years
Spheroid
45
1.0 long?
0.8 dia?
1992 Jun 5.3
2001 Dec 19.90
74.01
74.00
115.21
115.17
7841
7841
1447
1445
1480
1480
0.002
0.002
114
281
Cosmos 2194 *
[Cosmos]
1992-30 H
(21983)
1992 Jun 3.04
10000 years
Spheroid
45
1.0 long?
0.8 dia?
1992 Jun 5.4
2001 Dec 19.98
74.00
74
115.40
115.35
7850
7850
1459
1457
1485
1480
0.002
0.002
147
333
Cosmos 2187
2nd stage
1992-30 J
(21984)
1992 Jun 3.04
20000 years
Cylinder
2200?
7.4 long
2.4 dia
1992 Jun 6.5
2001 Dec 19.89
74.00
73.99
117.89
117.82
7963
7961
1480
1484
1689
1681
0.013
0.012
262
340
*
Strela-1 M satellite
2004 December 31 – version 1.01
RAE Table of Earth Satellites
Year of Launch 1992
Name
[Launcher]
Fragments
Cospar ID
[Norad #] Launchsite
Cospar ID
(Revised 2001)
Launchdate
Lifetime + Descent date
[Norad]
Shape and
weight (kg)
Descent date
Size
(m)
Lifetime
Date of
orbital
determination
Orbital
Inclination
(deg)
Nodal
period
(min)
Semi
major axis
(km)
Page 1091
Perigee
height
(km)
Apogee
height
(km)
Orbital
Argument
eccentricity of perigee
(deg)
EUVE*
[Delta 6920-10
#210
1992-31 A
(21987)
CC-LC17A
1992 Jun 7.69
9 years
Box +
panels
3280
4.5 x
2.2 x
2.4
4.6 span
1992 Jun 8.0
2001 Dec 22.50
28.43
28.43
94.87
90.88
6900
6696
514
315
529
321
0.001
0.0004
194
126
Delta 2
second stage
1992-31 B
(21988)
1992 Jun 7.69
131 days
1992 Oct 16
Cylinder
6983 full
919 empty
5.88 long
2.44 dia
1992 Jun 8.4
30.21
92.45
6782
282
525
0.018
313
NSS K #
[Atlas 2A AC-105
Centaur II 8105}
1992-32 A
(21989)
CC-LC36B
1992 Jun 10.00
>million
years
Box +
panels
1780 full
1.52
3.18
2.03
19.3
1992
1992
1992
1992
2001
11.2
13.8
17.9
9.3
18.01
17.59
6.32
2.69
0.13
0.08
690.25
905.61
1100.53
1435.90
1436.13
25880
31010
35313
42163
42165
3139
13373
22065
35773
35776
35866
35891
35804
35797
35798
0.632
0.363
0.195
0.0003
0.0003
181
180
181
169
122
Atlas 2A
Centaur 105 stage
1992-32 B
(21990)
1992 Jun 10.00
30 years
Cylinder
2000?
10.1 long
3.05 dia
1992 Jun 20.2
2001 Dec 22.01
26.45
26.34
626.79
207.18
24273
11599
202
150
35589
10290
0.729
0.437
185
279
D
R
Resurs-F 15
[Soyuz 11A511U]
1992-33 A
(21998)
PLE-LC43/3
1992 Jun 23.33
15.9 days
1992 Jul 9.2
Sphere-cone
6300
6.5 long?
2.4 dia
1992 Jun 24.6
82.32
89.15
6608
226
233
0.0005
288
D
Resurs-F 15
Block I 3rd stage
1992-33 B
(21999)
1992 Jun 23.33
2 days
1992 Jun 25
Cylinder
2500?
7.5 long
2.6 dia
1992 Jun 23.6
82.32
88.48
6575
178
215
0.003
108
D
Resurs-F 15
engine
1992-33 E
(22030)
1992 Jun 23.33
28 days
1992 Jul 21
Cone
600?
full
1.9 long
1.0 dia
1992 Jun 10.0
82.32
89.04
6602
222
226
0.0003
138
D
D
D
Fragment
Fragment
Fragment
1992-33 C
1992-33 D
1992-33 F
[22026]
[22029]
[22031]
1992 Jul 12
1992 Jul 11
1992 Jul 10
19 days
18 days
17 days
1992-34A
(22000)
CC-LC39A
1992 Jun 25.68
13.81 days
1992 Jul 9.49
Cylinder +
delta wing
103812
empty
37.1 long
17.4 high
23.8 span
1992 Jun 26.1
1992 Jul 8.8
28.47
28.47
90.38
89.78
6681
6651
300
245
305
301
0.0004
0.004
349
84
D
D STS 50**
7M (Columbia F12)
R [Shuttle]
wide?
high?
long?
span?
Jun
Jun
Jun
Jul
Dec
* Extreme Ultraviolet Explorer
** Launch and landing at Cape Canaveral (2 women, 5 men). Cargo bay carried US Microgravity Laboratory, USML-1, and the
Extended Duration Orbiter (EDO) kit (not separated).
# Renamed from Intelsat K after being bought by New Skies Satellites.
2004 December 31 – version 1.01
RAE Table of Earth Satellites
Year of Launch 1992
Name
[Launcher]
Fragments
Cospar ID
[Norad #] Launchsite
Cospar ID
(Revised 2001)
Launchdate
Lifetime + Descent date
[Norad]
Shape and
weight (kg)
Descent date
Size
(m)
Lifetime
Date of
orbital
determination
Orbital
Inclination
(deg)
Nodal
period
(min)
Semi
major axis
(km)
Page 1092
Perigee
height
(km)
Apogee
height
(km)
Orbital
Argument
eccentricity of perigee
(deg)
D
Progress-M 13**
[Soyuz 11A511U2
15000-062
1992-35 A
(22004)
BAI-LC31
1992 Jun 30.70
23.64 days
1992 Jul 24.34
Spherecylinder +
2 panels
7320
7.9 long?
2.3 dia?
1992 Jul 2.6
1992 Jul 4.0
51.60
51.60
90.87
92.51
6699
6779
309
391
332
411
0.002
0.001
245
253
D
Progress-M 13
Block I 3rd stage
1992-35 B
(22005)
1992 Jun 30.70
2 days
1992 Jul 2
Cylinder
2500?
7.5 long?
2.6 dia?
1992 Jun 30.8
51.63
88.47
6580
181
222
0.003
116
Cosmos 2195
[Cosmos 11K65M
65072-427]
1992-36 A
(22006)
PLE
1992 Jul 1.85
1200 years
Cylinder
810
2.1 long
2.0 dia
1992 Jul 3.1
2001 Dec 19.71
82.93
82.93
104.85
104.75
7363
7361
958
955
1011
1011
0.004
0.004
288
20
Cosmos 2195
2nd stage
1992-36 B
(22007)
1992 Jul 1.85
600 years
Cylinder
2200?
7.4 long
2.4 dia
1992 Jul 3.0
2001 Dec 19.95
82.93
82.93
104.66
104.53
7354
7351
954
950
998
959
0.003
0.003
279
336
DSCS 3B-02
(USA 82)
[Atlas 2 AC-103
Centaur II 8103]
1992-37 A
(22009)
CC-LC36A
1992 Jul 2.91
>million
years?
Box +
2 vanes?
1150 full?
875 empty?
2 long?
2.7 dia?
No elements available
Atlas 2
Centaur 103 stage
1992-37 B
(22010)
1992 Jul 2.91
3637 days
2002 Jun 17
Cylinder
2000?
10.1 long
3.05 dia
2002 Jun 16.77
0.031
32
IABS-02
1992-37C
(22011)
1992 Jul 2.91
>million
years?
-
-
SAMPEX**
[Scout G-1 S215C]
1992-38 A
(22012)
VDB-SLC5
1992 Jul 3.60
20 years
Box +
panels
158
1.4? x
0.9? x
0.6?
3.0? span
1992 Jul 5.3
2001 Dec 21.92
81.67
81.65
96.81
95.40
6981
6916
515
475
691
600
0.013
0.009
200
20
Altair
Scout 4th stage
1992-38 B
(22013)
1992 Jul 3.60
10 years
Cylinder
24
1.50 long
0.46 dia
1992 Jul 6.1
2001 Dec 22.41
81.67
81.63
96.78
91.87
6980
6745
515
343
688
389
0.012
0.003
197
267
Fragment
Fragment
1992-38 C
1992-38 D
[22847]
[22848]
1999 Nov 24.24 2691.64 days1993 Oct 5.49
1998 Jan 9
2016 days
1993 Oct 5.44
81.66
91.68
96.86
95.14
6987
6904
486
484
731
567
0.018
0.006
181
64
D
D
D
26.02
Orbital data not released
91.15
6709
121
540
Orbital data not released
No elements available
* Progress-M 13 docked with Mir (+X port) on 1992 Jul 4.70.
** Solar, Anomalous and Magnetospheric Particle Explorer
2004 December 31 – version 1.01
Orbital data not released
Undocked 1992 Jul 24.18 and de-orbited.
RAE Table of Earth Satellites
Year of Launch 1992
Name
[Launcher]
Fragments
D
Cospar ID
[Norad #] Launchsite
Cospar ID
(Revised 2001)
Launchdate
Lifetime + Descent date
[Norad]
Shape and
weight (kg)
Descent date
Size
(m)
Lifetime
Date of
orbital
determination
Orbital
Inclination
(deg)
Nodal
period
(min)
Page 1093
Semi
major axis
(km)
Perigee
height
(km)
Apogee
height
(km)
Orbital
Argument
eccentricity of perigee
(deg)
26670
26560
26561
20213
19960
19837
20367
20404
20528
0.003
0.008
0.013
194
274
17
7024
6983
564
539
728
669
0.012
0.009
227
200
GPS 2-14 (USA 83)
Navstar
[Delta 7925 #211]
1992-39 A
(22014)
CC-LC17B
1992 Jul 7.39
1 million
years
Cylinder +
4 vanes
1667 full
844 empty
2.4 long?
1.8 dia?
5.3 span?
1992 Jul 10.0
1992 Jul 19.5
2001 Dec 19.21
54.98
55.05
55.57
722.39
717.93
718.00
Delta 2
second stage
1992-39 B
(22015)
1992 Jul 7.39
20 years
Cylinder
6983 full
919 empty
5.88 long
2.44 dia
1992 Jul 11.4
2001 Dec 19.60
20.72
20.71
97.43
96.78
GPS 2-14
PAM-D PKM
1992-39 C
(22016)
1992 Jul 7.39
2695 days
1999 Nov 23
Cylinder
2154?
full
2.29 long
1.5 dia
1992 Jul 11.0
1999 Nov 23.32
34.71
34.63
356.97
88.72
16677
6589
188
113
20410
303
0.606
0.014
194
356
Fragment
1992-39 D
[23299]
2002 Jan 3.83
34.55
200.95
11365
192
9781
0.422
339
26289
26540
26581
590
590
3441
39232
39733
36964
0.735
0.737
0.631
318
318
280
Cosmos 2196
[Molniya
8K78M / 2BL]
1992-40 A
(22017)
PLE-LC43/3
1992 Jul 8.41
100 years?
Windmill +
6 vanes
1250?
4.2 long?
1.6 dia
1992 Jul 9.4
1992 Jul 10.9
2001 Dec 19.26
62.96
62.95
66.89
707.00
717.14
718.82
D
Cosmos 2196
Block I 3rd stage
1992-40 B
(22018)
1992 Jul 8.41
38 days
1992 Aug 15
Cylinder
2500?
7.5 long
2.6 dia
1992 Jul 8.9
62.78
92.33
6767
211
567
0.026
121
D
Cosmos 2196
4th stage casing
1992-40 C
(22019)
1992 Jul 8.41
18 days
1992 Jul 26
Irregular
-
1992 Jul 9.0
62.83
92.35
6768
179
602
0.031
124
Cosmos 2196
Block L 4th stage
1992-40 D
(22020)
1992 Jul 8.41
100 years?
Cylinder
440 empty
2.0 long
2.0 dia
1992 Jul 9.4
2001 Dec 20.21
62.93
66.85
707.04
705.70
26290
26257
589
3134
39235
36622
0.735
0.638
318
275
D
Cosmos 2196
Ullage motor
1992-40 E
[22021]
1992 Jul 8.41
6 days
1992 Jul 14
Ellipsoid
55
1.0 long
0.6 dia
1992 Jul 13.84
62.36
89.83
6644
222
309
0.007
117
D
Cosmos 2196
Ullage motor
1992-40 F
[22022]
1992 Jul 8.41
30 days
1992 Aug 7
Ellipsoid
55
1.0 long
0.6 dia
Insat 2A*
[Ariane 4-23]
1992-41 A
(22027)
KOU-ELA2
1992 Jul 9.95
>million
years
Box + boom
and sail +
panel
1162 full
911 empty
1.93 x
1.70 x
1.64
23 span
1992 Jul 10.8
1992 Aug 7.9
2001 Dec 18.86
0.38
0.19
3.62
35491
42213
42165
22392
35537
35774
35834
36132
35828
0.189
0.007
0.001
163
56
162
* Indian multipurpose satellite
2004 December 31 – version 1.01
1108.89
1438.43
1436.08
1992-41 continued on page 1094
RAE Table of Earth Satellites
Year of Launch 1992
Name
[Launcher]
Fragments
Cospar ID
[Norad #] Launchsite
Cospar ID
(Revised 2001)
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)
Perigee
height
(km)
Apogee
height
(km)
Orbital
Argument
eccentricity of perigee
(deg)
Eutelsat 2 F-4*
[Ariane 4-23]
1992-41 B
(22028)
1992 Jul 9.95
>million
years
Box +
panels
1123 full
921 empty
1.3 x
1.3 x
2.2
22.4 span
1992
1992
1992
2001
12.0
12.3
28.1
18.93
3.36
0.15
0.07
0.68
768.10
1342.66
1436.03
1436.00
27788
40318
42166
42163
7077
32086
35784
35770
35743
35793
35791
35799
0.516
0.046
0.0001
0.0003
179
173
260
152
Ariane 44L V51 ##
third stage
1992-41 C
(22032)
1992 Jul 9.95
20 years
Cylinder
11830 full
1280 empty
11.4 long
2.6 dia
1992 Jul 12.8
2001 Dec 20.37
7.23
7.11
636.08
468.75
24516
19989
231
230
36045
26991
0.730
0.669
181
209
D
Ariane 44L V51
Spelda top
1992-41 D
[22033]
1992 Jul 9.95
2853 days
2000 May 1
2000 Apr 24.97
7.25
104.42
7346
138
1796
0.113
30
D
Fragments
1992-41 E-H
4 pieces, all have decayed
For orbital information see extra pages at the end of the year
Cosmos 2197 #
[Tsiklon 3]
1992-42 A
(22034)
PLE-LC32
1992 Jul 13.74
10000 years
Cylinder +
boom
230
1.6 long?
0.8 dia?
1992 Jul 16.2
2001 Dec 19.94
82.59
82.59
113.99
113.92
7785
7785
1397
1396
1416
1416
0.001
0.001
21
99
Cosmos 2198 #
[Tsiklon]
1992-42 B
(22035)
1992 Jul 13.74
10000 years
Cylinder +
boom
230
1.6 long?
0.8 dia?
1992 Jul 18.6
2001 Dec 19.65
82.59
82.59
114.13
114.05
7791
7791
1410
1408
1416
1417
0.0004
0.0006
357
89
Cosmos 2199**
[Tsiklon]
1992-42 C
(22036)
1992 Jul 13.74
10000 years
Cylinder +
boom
230
1.6 long?
0.8 dia?
1992 Jul 17.6
2001 Dec 19.68
82.60
82.60
114.28
114.20
7798
7798
1414
1411
1426
1427
0.001
0.001
254
39
Cosmos 2200 #
[Tsiklon]
1992-42 D
(22037)
1992 Jul 13.74
10000 years
Cylinder +
boom
230
1.6 long?
0.8 dia?
1992 Jul 15.7
2001 Dec 19.65
82.59
82.59
114.07
114.00
7789
7788
1405
1404
1416
1416
0.001
0.0008
15
101
Cosmos 2201**
[Tsiklon]
1992-42 E
(22038)
1992 Jul 13.74
10000 years
Cylinder +
boom
230
1.6 long?
0.8 dia?
1992 Jul 22.5
2001 Dec 19.66
82.59
82.59
114.21
114.13
7795
7795
1413
1410
1421
1422
0.0005
0.0008
271
51
Cosmos 2202 #
[Tsiklon]
1992-42 F
(22039)
1992 Jul 13.74
10000 years
Cylinder +
boom
230
1.6 long?
0.8 dia?
1992 Jul 14.1
2001 Dec 19.93
82.59
82.59
114.14
114.05
7792
7791
1409
1406
1419
1418
0.001
0.0008
350
73
Cosmos 2197
3rd stage
1992-42 G
(22040)
1992 Jul 13.74
15000 years
Cylinder
2200?
7.4 long
2.4 dia
1992 Jul 15.1
2001 Dec 19.75
82.60
82.60
114.78
114.70
7821
7821
1412
1409
1474
1475
0.004
0.004
242
95
D
Fragment
1992-42 J
[27675]
2003 May 18
3961 days
*
#
**
##
European communications satellite
Strela-3 satellite
Payload in the demonstration phase of the commercial Gonets store-and-forward communications system.
Fragmented, see extra page 1992-2
2004 December 31 – version 1.01
Jul
Jul
Jul
Dec
Page 1094
Nodal
period
(min)
Gonets means "Messenger".
RAE Table of Earth Satellites
Year of Launch 1992
Name
[Launcher]
Fragments
Cospar ID
[Norad #] Launchsite
Cospar ID
Launchdate
Lifetime + Descent date
[Norad]
Shape and
weight (kg)
Descent date
Gorizont 26
1992-43 A
[Proton 8K82K
(22041)
371-02/11S861 60L] BAI-LC81L
1992 Jul 14.92
>million
years
Cylinder +
dish +
panels
2000?
D
Gorizont 26
third stage
1992-43 B
(22042)
1992 Jul 14.92
3 days
1992 Jul 17
D
Gorizont 26
4th stage casing
1992-43 C
(22043)
Gorizont 26
Block DM 2
fourth stage
D
D
(Revised 2001)
Date of
orbital
determination
Orbital
Inclination
(deg)
-
1992 Jul 14.9
1992 Jul 28.0
2001 Dec 21.94
1.50
1.48
5.53
Cylinder
6.5 long?
4 dia
1992 Jul 15.1
51.67
1992 Jul 14.92
1 day
1992 Jul 15
Irregular
-
1992 Jul 15.1
51.66
1992-43 D
(22044)
1992 Jul 14.92
>million
years
Cylinder
17300 full
5.5 long
4.0 dia
1992 Jul 25.9
2001 Dec 12.55
1.52
5.68
Gorizont 26
Ullage motor
1992-43 E
[22047]
1992 Jul 14.92
339 days
1993 Jun 18
Ellipsoid
55
1.0 long
0.6 dia
Gorizont 26
Ullage motor
1992-43 F
[22048]
1992 Jul 14.92
3296 days
2001 Jul 23
Ellipsoid
55
1.0 long
0.6 dia
2001 Jul 23.34
46.40
89.25
D? Geotail*
[Delta 6925 #212]
1992-44 A
(22049)
CC-LC17A
1992 Jul 24.60
87 days?
1992 Oct 19 A?
Cylinder +
booms
1008
1.6 long
2.2 dia
1992 Jul 24.6
28.65
12346.64
D
1992-44 B
(22050)
1992 Jul 24.60
235 days
1993 Mar 16
Cylinder
6983 full?
919 empty?
5.88 long
2.44 dia
1992 Jul 28.1
27.46
101.81
1992-44 C
(22051)
1992 Jul 24.60
160 days?
1993 Jan 1 A?
Cylinder
2154 full?
2.29 long
1.5 dia
1992 Jul 24.6
28.70
13359.69
Delta 2
second stage**
D? Geotail
PAM-D PKM
Size
(m)
Lifetime
* Japanese Institute for Space and Astronautical Sciences, ISAS.
** Carries DUVE, Diffuse Ultraviolet Experiment for University of California, Berkley.
2004 December 31 – version 1.01
Page 1095
Nodal
period
(min)
Semi
major axis
(km)
Perigee
height
(km)
Apogee
height
(km)
Orbital
Argument
eccentricity of perigee
(deg)
1476.02
1435.68
1436.03
42945
42159
42164
36479
35762
35775
36654
35799
35795
0.002
0.0004
0.0002
108
95
181
88.26
6570
188
195
0.0005
317
88.34
6574
188
203
0.001
96
42862
42862
36378
36380
36590
36587
0.002
0.002
52
315
6616
106
369
0.020
91
1471.76
1471.87
177020 185
341100 0.963
151
7231
1489
0.088
178
360211 0.965
151
218
186576 184
RAE Table of Earth Satellites
Year of Launch 1992
Name
[Launcher]
Fragments
Cospar ID
[Norad #] Launchsite
Cospar ID
(Revised 2001)
Launchdate
Lifetime + Descent date
[Norad]
Shape and
weight (kg)
Descent date
Size
(m)
Lifetime
Date of
orbital
determination
Orbital
Inclination
(deg)
Nodal
period
(min)
Semi
major axis
(km)
Page 1096
Perigee
height
(km)
Apogee
height
(km)
Orbital
Argument
eccentricity of perigee
(deg)
D
R
Cosmos 2203
[Soyuz 11A511U]
1992-45 A
(22052)
PLE
1992 Jul 24.82
60.0 days
1992 Sep 22.8
Spherecylinder
6700?
7 long?
2.4 dia
1992 Jul 25.2
62.81
89.53
6629
190
312
0.009
115
D
Cosmos 2203
Block I 3rd stage
1992-45 B
(22053)
1992 Jul 24.82
8 days
1992 Aug 1
Cylinder
2500?
7.5 long
2.6 dia
1992 Jul 24.9
62.79
89.44
6625
190
304
0.009
115
D
Fragment
1992-45 C
[22135]
1992 Sep 23
61 days
D Soyuz-TM 15*
3M [Soyuz 11A511U2]
R
1992-46 A
(22054)
BAI-LC1
1992 Jul 27.26
187.90 days
1993 Feb 01.16
Spherecylinder +
2 panels
7070
7.5 long
2.3 to
2.72 dia
1992 Jul 27.7
51.62
90.12
6662
223
344
0.009
115
D
1992-46 B
(22055)
1992 Jul 27.26
2 days
1992 Jul 29
Cylinder
2500?
7.5 long
2.6 dia
1992 Jul 27.9
51.63
88.33
6573
190
200
0.001
112
Cosmos 2204
1992-47 A
(Glonass 56)
(22056)
[Proton 8K82K
BAI-LC81L
376-01/11S861 63L]
1992 Jul 30.08
1 million
years
1400
Cylinder +
panels +
boom
-
1992 Aug 7.0
1992 Aug 27.1
2001 Dec 19.72
64.85
64.84
63.91
667.04
675.74
675.72
25289
25508
25508
18686
19121
19111
19135
19139
19147
0.009
0.0004
0.0007
238
269
253
Cosmos 2205
(Glonass 57)
[Proton]
1992-47 B
(22057)
1992 Jul 30.08
1 million
years
Cylinder +
panels +
boom
1400
-
L
1992 Jul 30.6
1992 Aug 10.8
2001 Dec 19.09
64.84
64.87
63.92
675.84
675.72
675.72
25511
25508
25508
19131
19117
19112
19134
19142
19146
0.0001
0.001
0.0007
104
236
325
Cosmos 2206
(Glonass 58)
[Proton]
1992-47 C
(22058)
1992 Jul 30.08
1 million
years
Cylinder +
panels +
boom
1400
-
L
1992 Aug 7.5
1992 Aug 19.9
2001 Dec 20.90
64.84
64.82
63.92
685.27
675.73
675.72
25747
25508
25508
19145
19103
19105
19593
19156
19153
0.009
0.001
0.0009
57
300
271
D
Cosmos 2204**
third stage
1992-47 D
(22059)
1992 Jul 30.08
<1 day
1992 Jul 30
Cylinder
6.5 long?
4 dia
1992 Jul 30.1
64.83
87.67
6537
151
167
0.001
267
D
Cosmos 2204**
4th stage casing
1992-47 E
[22060]
1992 Jul 30.08
< 1 day
1992 Jul 30
L
Soyuz-TM 15
Block I 3rd stage
* Soyuz TM15 docked with Mir (+X port) on 1992 Jul 29.33, with 2 CIS and 1 French cosmonaut, the Antares mission.
** Originally listed on page 1097
1992-47 continued on page 1097
2004 December 31 – version 1.01
RAE Table of Earth Satellites
Year of Launch 1992
Name
[Launcher]
Fragments
Cospar ID
[Norad #] Launchsite
Cospar ID
(Revised 2001)
Launchdate
Lifetime + Descent date
[Norad]
Shape and
weight (kg)
Descent date
Size
(m)
Lifetime
Date of
orbital
determination
Orbital
Inclination
(deg)
Nodal
period
(min)
Page 1097
Semi
major axis
(km)
Perigee
height
(km)
Apogee
height
(km)
Orbital
Argument
eccentricity of perigee
(deg)
Cosmos 2204
Block DM2
fourth stage
1992-47 F
(22061)
1992 Jul 30.08
1 million
years
Cylinder
17300 full
5.5 long
4.0 dia
1992 Aug 2.3
2001 Dec 19.00
64.61
63.91
675.03
675.00
25490
25490
19089
19098
19135
19124
0.001
0.0005
322
322
Cosmos 2204
Ullage motor
1992-47 G
[22066]
1992 Jul 30.08
Ellipsoid
55
1.0 long
0.6 dia
2001 Dec 21.04
64.67
338.75
16097
316
19121
0.584
187
Cosmos 2204 #
Ullage motor
1992-47 H
[22067]
1992 Jul 30.08
3064.30 days
2001 Dec 19.38
Ellipsoid
55
1.0 long
0.6 dia
2001 Dec 18.99
64.45
92.03
6753
259
490
0.018
182
Fragment
Fragment
Fragment
1992-47 J
1992-47 K
1992-47 L
[23616]
[24938]
[27805]
2001 Dec 17.81
2001 Dec 21.99
2004 Feb 3.64
64.43
64.40
65.90
331.28
337.68
282.75
15860
16064
14270
316
322
496
18646
19048
15287
0.578
0.582
0.518
208
211
18
D
R
Cosmos 2207
[Soyuz 11A511U]
1992-48 A
(22062)
PLE
1992 Jul 30.46
13.8 days
1992 Aug 13.3
Spherecylinder
6300?
6.5 long?
2.4 dia
1992 Jul 30.7
1992 Jul 31.7
1992 Aug 3.1
82.33
82.33
82.33
88.72
90.07
90.49
6586
6653
6674
182
232
237
235
317
355
0.004
0.006
0.009
94
85
57
D
Cosmos 2207
Block I 3rd stage
1992-48 B
(22063)
1992 Jul 30.46
2 days
1992 Aug 1
Cylinder
2500?
7.5 long
2.6 dia
1992 Jul 30.8
82.33
88.50
6575
176
218
0.003
96
D
Cosmos 2207
engine
1992-48 C
(22082)
1992 Jul 30.46
62 days
1992 Sep 30
Cone
600?
full
1.9 long
1.0 dia
1992 Aug 13.9
82.33
90.45
6672
236
351
0.009
54
D
Fragments
1992-48 D-G
4 pieces, all have decayed
D STS 46*
7M (Atlantis F12)
R [Shuttle]
1992-49 A
(22064)
CC-LC39B
1992 Jul 31.58
7.97 days
1992 Aug 8.55
Cylinder +
delta wing
94674
empty
37.1 long
17.4 high
23.8 span
1992 Aug 1.8
1992 Aug 4.7
1992 Aug 6.4
28.47
28.48
28.48
92.93
90.30
88.94
6805
6677
6610
422
296
228
433
302
236
0.001
0.0005
0.001
286
310
273
D
1992-49 B
(22065)
1992 Jul 31.58
334.96 days
1993 Jul 1.54
Box +
panels
4491 full
4.5? x
2.9? x
2.5?
20 span
1992
1992
1992
1992
1993
1993
28.47
28.46
28.46
28.46
28.46
28.46
93.10
93.29
94.14
94.52
94.40
94.17
6814
6823
6864
6883
6868
6857
431
428
467
502
463
475
441
461
505
507
516
482
0.001
0.002
0.003
0.0003
0.004
0.0005
83
125
325
254
282
186
D
Eureca-1**
#
*
For orbital information see extra pages at the end of the year
Aug
Aug
Aug
Aug
May
Jun
2.7
5.0
7.0
8.0
20.32
23.73
See extra page for information on the fragmentation.
Launch and landing at Cape Canaveral (1 woman, 6 men including a Swiss ESA mission specialist and an Italian
payload specialist). Cargo bay carried Tethered Satellite System, TSS-1, for Agenzia Spaziale Italiana, ASI,
not separated; deployed to 256 m "above" Shuttle and then reeled back.
** European Retrievable Carrier, ejected from Shuttle 1992 Aug 2.30. Retrieved by STS 57, 1993-37 A, on 1993 Jun 24.58 and returned to earth.
2004 December 31 – version 1.01
RAE Table of Earth Satellites
Year of Launch 1992
Name
[Launcher]
Fragments
Cospar ID
[Norad #] Launchsite
Cospar ID
(Revised 2001)
Launchdate
Lifetime + Descent date
[Norad]
Shape and
weight (kg)
Descent date
Size
(m)
Lifetime
Date of
orbital
determination
Orbital
Inclination
(deg)
Nodal
period
(min)
Semi
major axis
(km)
Page 1098
Perigee
height
(km)
Apogee
height
(km)
Orbital
Argument
eccentricity of perigee
(deg)
27028
26555
26556
617
632
1373
40682
39721
38981
0.741
0.736
0.708
288
288
251
Molniya-1 84
[Molniya
8K78M / ML]
1992-50 A
(22068)
PLE
1992 Aug 6.81
10 years?
Windmill +
6 vanes
1000?
3.4 long
1.6 dia
1992 Aug 7.9
1992 Aug 19.0
2001 Dec 20.87
62.87
62.85
64.64
737.00
717.73
717.77
D
Molniya-1 84
Block I 3rd stage
1992-50 B
(22069)
1992 Aug 6.81
45 days
1992 Sep 20
Cylinder
2500?
7.5 long
2.6 dia
1992 Aug 7.3
62.82
92.51
6766
216
579
0.027
123
D
Molniya-1 84
4th stage casing
1992-50 C
(22070)
1992 Aug 6.81
23 days
1992 Aug 29
Irregular
-
1992 Aug 7.1
62.82
92.54
6777
185
614
0.032
119
Molniya-1 84
Block L 4th stage
1992-50 D
(22071)
1992 Aug 6.81
15¾ years
Cylinder
440
empty
2.0 long
2.0 dia
1992 Aug 9.9
2001 Dec 18.62
62.84
64.93
733.54
733.35
26943
26938
623
1763
40507
39356
0.740
0.698
288
256
D
Molniya-1 84
Ullage motor
1992-50 E
[22095]
1992 Aug 6.81
2 days
1992 Aug 8
D
r
FSW-2 1 *
(China 35)
[CZ-2D #1]
1992-51 A
(22072)
JIUQ-LA2
1992 Aug 9.33
23 days
1992 Sep 1
Tapered
cylinder +
hemisphere
2500
4.9 long?
1.3 to
2.2 dia?
1992 Aug 9.7
1992 Aug 12.5
63.07
63.07
89.56
89.69
6631
6637
172
172
333
346
0.012
0.013
143
143
D
FSW-2 1
2nd stage
1992-51 B
(22073)
1992 Aug 9.33
7 days
1992 Aug 16
Cylinder
7.0 long
3.35 dia
1992 Aug 9.6
63.07
89.50
6628
170
329
0.012
143
D
D
D
Fragment
Fragment
Fragment#
1992-51 C
1992-51 D
1992-51 E
[22074]
[22075]
[23280]
1992 Aug 9
1992 Aug 10
1992 Aug 27
< 1 day
1 day
16 days
L
Topex/Poseidon**
[Ariane 4-24]
1992-52 A
(22076)
KOU-ELA2
1992 Aug 10.96
10000 years
Box +
panel
2402 full
2185 empty
4.15 x
2.19 x
1.45
8.7 span
1992 Aug 12.8
1992 Sep 17.0
2001 Dec 21.49
66.08
66.06
66.04
112.13
112.43
112.42
7702
7716
7716
1317
1332
1331
1331
1343
1344
0.001
0.001
0.0008
300
268
270
* Capsule returned to mid-Sichuan Province 1992 Aug 25.14.
** NASA/CNES to measure sea surface topography with high precision.
# Re-assigned from 1994-22 C per 2004 Nov.
2004 December 31 – version 1.01
1992-52 continued on page 1099
RAE Table of Earth Satellites
Year of Launch 1992
Name
[Launcher]
Fragments
D
Cospar ID
[Norad #] Launchsite
Cospar ID
(Revised 2001)
Launchdate
Lifetime + Descent date
[Norad]
Shape and
weight (kg)
Descent date
Size
(m)
Lifetime
Date of
orbital
determination
Orbital
Inclination
(deg)
Nodal
period
(min)
Semi
major axis
(km)
Page 1099
Perigee
height
(km)
Apogee
height
(km)
Orbital
Argument
eccentricity of perigee
(deg)
Uribyol 1*
(Kitsat,
Oscar 23)
[Ariane 4-24]
1992-52 B
(22077)
1992 Aug 10.96
10000 years
Box +
boom
50
0.60 x
0.35 x
0.35
1992 Aug 12.5
2001 Dec 19.92
66.08
66.09
111.96
111.93
7695
7694
1304
1312
1329
1319
0.002
0.0005
265
190
S80/T**
[Ariane 4-24]
1992-52 C
(22078)
1992 Aug 10.96
10000 years
Box +
boom
50
0.60 x
0.35 x
0.35
1992 Aug 12.8
2001 Dec 21.34
66.09
66.09
111.94
111.92
7693
7693
1302
1311
1328
1318
0.002
0.0005
263
168
Ariane 42P V52
3rd stage [H 10+]
1992-52 D
(22079)
1992 Aug 10.96
5000 years
Cylinder
11800 full
1293 empty
11.4 long
2.6 dia
1992 Aug 12.7
2001 Dec 20.66
66.07
66.07
112.72
112.70
7729
7729
1301
1299
1401
1401
0.006
0.007
150
30
Cosmos 2208
[Cosmos 11K65M
65078-421]
1992-53 A
(22080)
PLE
1992 Aug 12.24
120 years
Cylinder +
paddles
750?
2 long?
1 dia?
1992 Aug 12.6
2001 Dec 20.04
74.04
74.04
100.86
100.73
7176
7172
788
783
807
803
0.001
0.001
6
189
Cosmos 2208
2nd stage
1992-53 B
(22081)
1992 Aug 12.24
100 years
Cylinder
2200?
7.4 long
2.4 dia
1992 Aug 12.6
2001 Dec 20.46
74.04
74.04
100.74
100.57
7170
7164
779
759
804
812
0.002
0.004
35
238
Fragment
Fragment
1992-53 C
1992-53 D
[24974]
[25027]
2001`Dec 19.59
2001 Dec 21.40
74.06
74.03
101.07
100.62
7187
7166
792
786
825
789
0.002
0.0002
109
153
Optus B1***
[CZ-2E #2]
1992-54 A
(22087)
XI-LC2
1992 Aug 13.96
>million
years
Box +
panels
1272 empty
2.3 cube
22 span
1992
1992
1992
2001
10.76
0.43
0.28
0.04
799.00
1472.25
1436.04
1436.10
28528
42872
42166
42165
7064
35657
35675
35770
37236
37330
35900
35803
0.529
0.020
0.003
0.0004
181
211
231
169
CZ-2E second
stage
1992-54B
(22088)
1992 Aug 13.96
121 days
1992 Dec 12
Cylinder
15.52 long
3.35 dia
1992 Aug 16.2
27.99
96.86
6996
203
1032
0.059
153
Optus B1
Star 63F PKM
1992-54C
(22089)
1992 Aug 13.96
1000 years
Sphere-cone
7900 full?
3600 empty?
2.69 long
1.60 dia
1992 Aug 16.6
2001 Dec 20.00
23.47
22.64
663.92
656.37
25223
25018
376
365
37313
36914
0.732
0.730
181
119
Aug
Aug
Sep
Dec
16.6
19.6
20.6
17.39
* Korean Advanced Institute of Technology, Seoul, microsat installed on ASAP, also known as Kitsat-1.
** CNES microsat to study use of the VHF band for mobile communications installed on ASAP.
*** Domestic satellite for Optus Communications, Australia, originally known as Aussat B1.
2004 December 31 – version 1.01
Uribyol means `Our Sun'.
RAE Table of Earth Satellites
Year of Launch 1992
Name
[Launcher]
Fragments
Cospar ID
[Norad #] Launchsite
Cospar ID
(Revised 2001)
Launchdate
Lifetime + Descent date
[Norad]
Shape and
weight (kg)
Descent date
Size
(m)
Lifetime
Date of
orbital
determination
Orbital
Inclination
(deg)
Nodal
period
(min)
Semi
major axis
(km)
Page 1100
Perigee
height
(km)
Apogee
height
(km)
Orbital
Argument
eccentricity of perigee
(deg)
D
r
Progress-M 14*
[Soyuz 11A511U2
U15000-064]
1992-55 A
(22090)
BAI-LC31
1992 Aug 15.93
67.08 days
1992 Oct 22.01
Spherecylinder +
2 panels
7020?
7.9 long?
2.3 dia?
1992 Aug 17.2
51.63
90.87
6698
288
352
0.005
114
D
Progress-M 14
Block I 3rd stage
1992-55 B
(22091)
1992 Aug 15.93
3 days
1992 Aug 18
Cylinder
2500?
7.5 long?
2.6 dia?
1992 Aug 16.2
51.62
88.45
6579
183
218
0.003
90
D
Fragment
1992-55 C
[22092]
1992 Aug 17
2 days
D
R
Resurs-F 16**
[Soyuz 11A511U]
1992-56 A
(22093)
PLE-LC16
1992 Aug 19.43
15.9 days
1992 Sep 4.3
Sphere-cone
6300
6.5 long?
2.4 dia
1992 Aug 20.9
82.57
89.15
6608
221
238
0.001
280
D
Resurs-F 16
Block I 3rd stage
1992-56 B
(22094)
1992 Aug 19.43
2 days
1992 Aug 21
Cylinder
2500?
7.5 long
2.6 dia
1992 Aug 19.9
82.57
88.49
6575
178
215
0.003
95
D
Pion 5***
[Soyuz]
1992-56 C
(22099)
1992 Aug 19.43
37 days
1992 Sep 25
Sphere
50?
0.33 dia
1992 Sep 1.7
82.56
89.12
6606
223
233
0.001
256
D
Pion 6†
[Soyuz]
1992-56 D
(22100)
1992 Aug 19.43
36 days
1992 Sep 24
Sphere
50?
0.33 dia
1992 Sep 2.7
82.57
89.11
6606
222
233
0.001
250
D
Resurs-F 16
engine
1992-56 E
(22102)
1992 Aug 19.43
25 days
1992 Sep 13
Cone
600?
full
1.9 long
1.0 dia
1992 Sep 4.7
82.56
89.05
6603
219
230
0.001
245
D
D
D
Fragment
Fragment
Fragment
1992-56 F
1992-56 G
1992-56 H
[22103]
[22104]
[22105]
1992 Sep 7
1992 Sep 7
1992 Sep 7
19 days
19 days
19 days
*
Progress-M 14 docked with Kvant 1 (-X port) on 1992 Aug 18.01. Undocked 1992 Oct 21.70 and de-orbited.
capsule landed in Kazakhstan 1992 Oct 22.01.
** Carried BINRAD, Beryllium-7 Induced Radiation experiment, for the US Naval Research Laboratory.
*** Passive satellite separated from Resurs-F 16, 1992 Sep 1.
† Passive satellite separated from Resurs-F 16, 1992 Sep 2.
2004 December 31 – version 1.01
A ballistic
RAE Table of Earth Satellites
Year of Launch 1992
Name
[Launcher]
Fragments
D
Cospar ID
[Norad #] Launchsite
Cospar ID
(Revised 2001)
Launchdate
Lifetime + Descent date
[Norad]
Shape and
weight (kg)
Descent date
Size
(m)
Lifetime
Date of
orbital
determination
Orbital
Inclination
(deg)
Sep
Sep
Nov
Dec
Page 1101
Nodal
period
(min)
Semi
major axis
(km)
Perigee
height
(km)
Apogee
height
(km)
Orbital
Argument
eccentricity of perigee
(deg)
42370
42051
42164
42165
35815
35470
35773
35778
36168
35877
35798
35165
0.004
0.005
0.0003
0.0002
232
119
115
328
Satcom C4*
[Delta 7925 #213]
1992-57 A
(22096)
CC-LC17B
1992 Aug 31.45
>million
years
Box +
panels
1169 full?
682 empty?
3.5 high?
15.7 span?
1992
1992
1992
2001
4.5
6.5
3.3
20.13
0.10
0.09
0.08
0.008
1446.48
1430.19
1435.95
1436.10
Delta 2
second stage
1992-57 B
(22097)
1992 Aug 31.45
100000 years
Cylinder
6983 full
919 empty
5.88 long
2.44 dia
1992 Sep 1.6
2001 Dec 19.94
25.21
25.21
131.69
131.85
8582
8582
1773
1766
2635
2640
0.050
0.051
4
301
Satcom C4
PAM-D PKM
1992-57 C
(22098)
1992 Aug 31.45
1 million
years
Cylinder
2154 full?
2.29 long
1.5 dia
1992 Sep 2.3
2001 Dec 13.63
20.33
19.79
661.52
661.90
25159
25159
1785
1826
35777
35735
0.676
0.674
359
182
GPS 2-15 (USA 84)
(Navstar 25)
[Delta 7925 #214]
1992-58 A
(22108)
CC-LC17A
1992 Sep 9.37
1 million
years
Cylinder +
4 vanes
1667 full
844 empty
2.4 long?
1.8 dia?
5.3 span?
1992 Sep 14.2
1992 Sep 29.3
2001 Dec 18.63
54.79
54.76
54.02
722.94
717.98
717.97
26683
26561
26560
19980
19907
19772
20630
20459
20591
0.012
0.010
0.015
99
121
216
Delta 2
second stage
1992-58 B
(22109)
1992 Sep 9.37
40 years
Cylinder
6983 full
919 empty
5.88 long
2.44 dia
1992 Sep 15.3
2001 Dec 20.15
19.79
19.78
98.37
98.22
7069
7052
659
643
724
703
0.005
0.004
228
81
GPS 2-15
PAM-D PKM
1992-58 C
(22110)
1992 Sep 9.37
1553 days
1996 Dec 10
Cylinder
2154?
full
2.29 long
1.5 dia
1992 Sep 12.2
34.72
355.68
16637
185
20333
0.606
195
Fragment
Fragment
1992-58 D
1992-58 E
[23300]
[26851]
1994 Oct 30.89
2004 Dec 30.64
19.81
34.86
96.54
237.00
6971
12687
551
221
635
12394
0.006
0.480
230
156
1992
1992
1992
2001
1.35
1.33
1.17
5.60
1445.99
1438.53
1436.12
1437.70
42360
42214
42167
42196
35907
35767
35766
35807
36057
35906
35812
35828
0.002
0.002
0.001
0.0002
191
17
20
249
Cosmos 2209
1992-59 A
[Proton 8K82K
(22112)
363-01/11S861 61L] BAI-LC81L
1992 Sep 10.75
>million
years
-
-
D
Cosmos 2209
third stage
1992-59 B
(22113)
1992 Sep 10.75
3 days
1992 Sep 13
Cylinder
6.5 long?
4 dia
1992 Sep 10.8
51.62
88.28
6571
186
199
0.001
6
D
Cosmos 2209
4th stage casing
1992-59 C
(22114)
1992 Sep 10.75
1 day
1992 Sep 11
Irregular
-
1992 Sep 11.0
51.64
88.01
6557
173
185
0.001
74
*
GE American Communications satellite
2004 December 31 – version 1.01
Sep
Sep
Nov
Dec
13.8
15.8
20.7
15.25
1992-59 continued on page 1102
RAE Table of Earth Satellites
Year of Launch 1992
Name
[Launcher]
Fragments
Cospar ID
[Norad #] Launchsite
Cospar ID
(Revised 2001)
Launchdate
Lifetime + Descent date
[Norad]
Shape and
weight (kg)
Descent date
Size
(m)
Lifetime
Date of
orbital
determination
Orbital
Inclination
(deg)
1992 Sep 12.8
2001 Dec 15.95
Cosmos 2209
Block DM2
fourth stage
1992-59 D
(22115)
1992 Sep 10.75
>million
years
Cylinder
17300
full
5.5 long
4.0 dia
D
Cosmos 2209
Ullage motor
1992-59 E
[22125]
Ellipsoid
55
1.0 long
0.6 dia
D
Cosmos 2209
Ullage motor
1992-59 F
[22126]
1992 Sep
192 days
1993 Mar
1992 Sep
229 days
1993 May
Ellipsoid
55
1.0 long
0.6 dia
10.75
31
10.75
Page 1102
Nodal
period
(min)
Semi
major axis
(km)
Perigee
height
(km)
Apogee
height
(km)
Orbital
Argument
eccentricity of perigee
(deg)
1.35
5.61
1442.67
1442.80
42295
42296
35881
35881
35953
35953
0.001
0.0009
229
105
7
Hispasat 1A*
[Ariane 4-25]
1992-60 A
(22116)
KOU-ELA2
1992 Sep 10.96
>million
years
Box +
panels
1325 full
1013 empty
2.5 x
2.2 x
2.2
22.3 span
1992
1992
1992
2001
Sep
Sep
Sep
Dec
14.2
20.1
27.1
19.84
2.63
0.08
0.03
0.06
833.96
1430.85
1436.24
1436.10
29353
42064
42170
42165
10235
35612
35783
35777
35716
35760
35800
35795
0.434
0.002
0.0002
0.0002
179
275
152
93
Satcom C3**
[Ariane 4-25]
1992-60 B
(22117)
1992 Sep 10.96
>million
years
Box +
panels
784 full
618 empty
1.5 x
1.6 x
1.0
15.1 span
1992
1992
1992
2001
Sep
Sep
Sep
Dec
14.4
15.4
25.4
21.11
0.16
0.13
0.12
0.08
1441.00
1437.80
1435.73
1436.10
42263
42200
42160
42165
35690
35693
35773
35775
36079
35951
35790
35798
0.005
0.003
0.0002
0.0003
218
208
27
130
D
Ariane 44LP V53
3rd stage [H 10+]
1992-60 C
(22118)
Cylinder
12108 full
1237 empty
11.7 long
2.6 dia
1992 Sep 12.5
6.88
640.73
24636
229
36286
0.732
179
D
Ariane 44LP V53
Spelda top
1992-60 D
[22119]
Fragment
1992-60 E
1992 Sep
405 days
1993 Oct
1992 Sep
559 days
1994 Mar
[25668]
1999 Apr 7.23
7.25
552.34
22300
256
31587
0.703
125
1992-61 A
(22120)
CC-LC39B
1992 Sep 12.60
7.94 days
1992 Sep 20.54
Cylinder +
delta wing
99449
empty
37.1 long
17.4 high
23.8 span
1992 Sep 12.9
57.00
90.58
6683
299
310
0.001
281
1992-62 A
(22133)
PLE
1992 Sep 22.67
59.1 days
1992 Nov 20.8
Spherecylinder
6700?
7 long?
2.4 dia
1992 Sep 26.2
67.16
89.76
6640
175
349
0.013
85
1992-62 B
(22134)
1992 Sep 22.67
4 days
1992 Sep 26
Cylinder
2500?
7.5 long
2.6 dia
1992 Sep 22.9
67.17
89.63
6634
163
348
0.014
99
D STS 47†
7M (Endeavour F2)
R [Shuttle]
D
R
Cosmos 2210
[Soyuz 11A511U]
D
Cosmos 2210
Block I 3rd stage
10.96
20
10.96
23
* Communications satellite for Hispasat SA, Spain
** GE American Communications satellite
*** Probably upper half of Spelda, Ariane's multiple launch system.
† Launch and landing at Cape Canaveral (2 women, 5 men including a Japanese payload specialist).
Spacelab-J (not separated).
2004 December 31 – version 1.01
Cargo bay carried
RAE Table of Earth Satellites
Year of Launch 1992
Name
[Launcher]
Fragments
Cospar ID
[Norad #] Launchsite
Cospar ID
Launchdate
Lifetime + Descent date
[Norad]
Shape and
weight (kg)
Descent date
Size
(m)
Lifetime
Date of
orbital
determination
(Revised 2001)
Orbital
Inclination
(deg)
Nodal
period
(min)
Semi
major axis
(km)
Page 1103
Perigee
height
(km)
Apogee
height
(km)
Orbital
Argument
eccentricity of perigee
(deg)
Mars Observer
[Titan 3 CT-4]
1992-63 A
(22136)
CC-LC40
1992 Sep 25.71
Titan 3
second stage
1992-63 B
(22137)
1992 Sep 25.71
6 days
1992 Oct 1
Mars Observer
Transfer Orbit
Stage (Orbus 21)
1992-63 C
(22138)
1992 Sep 25.71
Freja*
[CZ-2C #13]
1992-64 A
(22161)
JIUQ-LA2
1992 Oct 6.26
250 years
Conical
disc
214
1.10 to
2.20 dia
0.52 high
D
r
FSW-1 13 **
(China 38)
[CZ-2C]
1992-64 B
(22162)
1992 Oct 6.26
25 days
1992 Oct 31
Frustum +
hemisphere
2100
D
Freja
2nd stage
1992-64 C
(22163)
1992 Oct 6.26
14 days
1992 Oct 20
Cylinder
D
Fragments
1992-64D-K
7 pieces, all have decayed
D
R
Foton 5***
[Soyuz 11A511U]
1992-65 A
(22173)
PLE-LC43/3
1992 Oct 8.79
15.60 days
1992 Oct 24.39
Spherecylinder
6057
5.0 long
2.4 dia
1992 Oct 9.7
62.81
90.31
6668
220
359
0.010
108
D
Foton 5
Block I 3rd stage
1992-65 B
(22174)
1992 Oct 8.79
14 days
1992 Oct 22
Cylinder
2500?
7.5 long
2.6 dia
1992 Oct 9.5
62.80
90.18
6662
219
348
0.010
103
D
Foton 5
engine
1992-65 C
(22199)
1992 Oct 8.79
43 days
1992 Nov 20
Cone
600?
full
1.9 long
1.0 dia
1992 Oct 24.6
62.81
90.05
6655
216
339
0.009
110
D
Fragments
1992-65 D-F
3 pieces, all have decayed
D
Mars orbit? Lost contact during orbit insertion burn 1993 Aug 21
Most probably flew past Mars 1993 Aug 24
Cylinder
9.85 long
3.05 dia
1992 Sep 25.8
29.38
90.96
6709
143
519
0.028
164
1992 Oct 7.3
2001 Dec 20.50
63.01
62.99
108.97
108.55
7557
7538
596
556
1762
1764
0.077
0.080
260
185
1.55 long?
1.40 to
2.25 dia?
1992 Oct 7.6
63.01
89.76
6641
215
311
0.007
159
7.0 long
3.35 dia
1992 Oct 7.6
63.01
89.67
6637
213
304
0.007
159
Mars orbit?
For orbital information see extra pages at the end of the year
* Swedish auroral and magnetospheric satellite
** Transmitted until 1992 Oct 21. Capsule returned to SW Sichuan Province on 1992 Oct 13.19.
*** Microgravity materials processing. Carried the German payload, Biopan.
2004 December 31 – version 1.01
1992-66 continued on page 1104
RAE Table of Earth Satellites
Year of Launch 1992
Name
[Launcher]
Fragments
Cospar ID
[Norad #] Launchsite
Cospar ID
(Revised 2001)
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)
Perigee
height
(km)
Apogee
height
(km)
Orbital
Argument
eccentricity of perigee
(deg)
25072
42262
42166
42164
1517
35775
35778
35779
35871
35993
35797
35792
0.685
0.003
0.0002
0.0002
359
193
303
339
DFS 3†
(Kopernikus 3)
[Delta 7925 #215]
1992-66 A
(22175)
CC-LC17B
1992 Oct 12.41
>million
years
Box +
panels
1422 full
645 empty
3.4 x
2.0 x
1.7
15.4 span
1992
1992
1992
2001
12.5
16.3
19.0
18.93
19.77
0.07
0.05
0.02
658.07
1440.98
1436.04
1436.07
Delta 2
second stage
1992-66 B
(22176)
1992 Oct 12.41
100000 years
Cylinder
6983 full
919 empty
5.88 long
2.44 dia
1992 Oct 13.1
2001 Dec 19.25
25.08
25.09
132.47
132.65
8616
8616
1406
1406
3070
3069
0.097
0.096
19
122
DFS 3
PAM-D PKM
1992-66 C
(22177)
1992 Oct 12.41
1 million
years
Cylinder
2154 full?
2.29 long
1.5 dia
1992 Oct 12.5
2001 Dec 18.81
19.69
19.04
657.73
658.33
25064
25068
1510
1487
35861
35893
0.685
0.686
359
288
Molniya-3 42
[Molniya
8K78M / ML]
1992-67 A
(22178)
PLE-LC43/3
1992 Oct 14.83
10 years?
Windmill +
6 vanes
1000?
3.4 long
1.6 dia
1992
1992
1992
2001
62.83
62.83
62.84
63.96
736.66
718.21
717.75
717.83
27019
26566
26555
26557
455
461
477
2200
40827
39916
39877
38157
0.747
0.743
0.742
0.677
280
280
280
264
D
Molniya-3 42
Block I 3rd stage
1992-67 B
(22179)
1992 Oct 14.83
14 days
1992 Oct 28
Cylinder
2500?
7.5 long
2.6 dia
1992 Oct 16.2
62.82
90.32
6668
209
371
0.012
134
D
Molniya-3 42
4th stage casing
1992-67 C
(22180)
1992 Oct 14.83
10 days
1992 Oct 24
Irregular
-
1992 Oct 16.1
62.81
90.64
6684
182
431
0.019
123
Molniya-3 42
Block L 4th stage
1992-67 D
(22181)
1992 Oct 14.83
20 years
Cylinder
440
empty
2.0 long
2.0 dia
1992 Oct 19.5
2001 Dec 20.06
62.84
64.25
733.72
733.58
26947
26944
458
2406
40681
38724
0.746
0.674
280
267
Molniya-3 42
Ullage motor
1992-67 E
[22193]
Cosmos 2211 *
[Tsiklon 3]
Cylinder +
boom
230
1.6 long?
0.8 dia?
1992 Oct 21.4
2001 Dec 19.82
82.59
82.59
114.00
113.93
7785
7785
1400
1401
1415
1412
0.001
0.0007
32
348
Cosmos 2212 *
[Tsiklon]
1992-68 A
(22182)
PLE-LC32
1992-68 B
(22183)
1992 Oct 14.83
?
?
1992 Oct 20.54
10000 years
1992 Oct 20.54
10000 years
Cylinder +
boom
230
1.6 long?
0.8 dia?
1992 Oct 23.1
2001 Dec 19.84
82.59
82.59
114.09
114.02
7789
7789
1408
1408
1414
1413
0.0004
0.0003
31
12
Cosmos 2213 *
[Tsiklon]
1992-68 C
(22184)
1992 Oct 20.54
10000 years
Cylinder +
boom
230
1.6 long?
0.8 dia?
1992 Oct 23.5
2001 Dec 19.93
82.59
82.60
114.13
114.07
7791
7791
1409
1412
1418
1413
0.001
0.00001
309
276
Cosmos 2214 *
[Tsiklon]
1992-68 D
(22185)
1992 Oct 20.54
10000 years
Cylinder +
boom
230
1.6 long?
0.8 dia?
1992 Oct 22.1
2001 Dec 19.88
82.59
82.59
114.23
144.15
7796
7795
1414
1412
1422
1422
0.001
0.0006
246
226
D
*
Strela-3 satellite
2004 December 31 – version 1.01
Oct
Oct
Oct
Dec
Page 1104
Nodal
period
(min)
Oct
Oct
Nov
Dec
16.9
21.5
1.9
20.65
† Multi-purpose communications satellite for Deutsche Bundespost Telekom.
1992-68 continued on page 1105
RAE Table of Earth Satellites
Year of Launch 1992
Name
[Launcher]
Fragments
Cospar ID
[Norad #] Launchsite
Cospar ID
(Revised 2001)
Launchdate
Lifetime + Descent date
[Norad]
Shape and
weight (kg)
Descent date
Size
(m)
Lifetime
Date of
orbital
determination
Orbital
Inclination
(deg)
Nodal
period
(min)
Semi
major axis
(km)
Page 1105
Perigee
height
(km)
Apogee
height
(km)
Orbital
Argument
eccentricity of perigee
(deg)
Cosmos 2215 #
[Tsiklon]
1992-68 E
(22186)
1992 Oct 20.54
10000 years
Cylinder +
boom
230
1.6 long?
0.8 dia?
1992 Oct 22.4
2001 Dec 19.89
82.60
82.60
114.29
114.22
7799
7798
1413
1412
1428
1427
0.001
0.001
238
234
Cosmos 2216 #
[Tsiklon]
1992-68 F
(22187)
1992 Oct 20.54
10000 years
Cylinder +
boom
230
1.6 long?
0.8 dia?
1992 Oct 23.5
2001 Dec 21.30
82.60
82.59
114.14
114.07
7792
7791
1410
1411
1417
1415
0.0004
0.0003
4
258
Cosmos 2211
3rd stage
1992-68 G
(22188)
1992 Oct 20.54
15000 years
Cylinder
2200?
7.4 long
2.4 dia
1992 Oct 25.5
2001 Dec 19.98
82.60
82.60
114.81
114.75
7823
7822
1410
1409
1479
1478
0.004
0.004
232
321
Cosmos 2217
[Molniya
8K78M / 2BL]
1992-69 A
(22189)
PLE-LC16/2
1992 Oct 21.43
100 years?
Windmill +
6 vanes
1900
4.2 long?
1.6 dia
1992 Oct 22.0
1992 Oct 23.9
2001 Dec 20.97
62.94
62.95
67.15
708.92
717.79
716.47
26337
26556
26531
596
599
3885
39321
39757
36420
0.735
0.737
0.613
318
318
257
D
Cosmos 2217
Block I 3rd stage
1992-69 B
(22190)
1992 Oct 21.43
35 days
1992 Nov 25
Cylinder
2500?
7.5 long
2.6 dia
1992 Oct 22.4
62.82
92.54
6777
213
585
0.027
119
D
Cosmos 2217
4th stage casing
1992-69 C
(22191)
1992 Oct 21.43
17 days
1992 Nov 7
Irregular
1992 Oct 22.1
62.86
92.49
6775
181
613
0.032
122
Cosmos 2217
Block L 4th stage
1992-69 D
(22192)
1992 Oct 21.43
100 years?
Cylinder
440 empty
2.0 long
2.0 dia
1992 Oct 22.5
2001 Dec 20.35
63.33
67.39
710.13
710.03
26366
26364
603
2937
39374
37034
0.735
0.647
318
241
D STS 52*
6M (Columbia F13)
R [Shuttle]
1992-70 A
(22194)
CC-LC39B
1992 Oct 22.72
9.87 days
1992 Nov 1.59
Cylinder +
delta wing
97200
empty
37.1 long
17.4 high
23.8 span
1992 Oct 23.0
1992 Oct 24.3
1992 Nov 1.3
28.46
28.47
28.47
90.39
90.11
88.51
6681
6667
6588
302
285
206
304
293
215
0.0002
0.001
0.001
184
281
315
L
Lageos 2**
1992-70 B
(22195)
1992 Oct 22.72
>million
years
Sphere
405
0.60 dia
1992 Oct 25.5
2001 Dec 19.89
52.64
52.64
222.42
222.45
12162
12162
5617
5616
5950
5951
0.014
0.014
215
237
D
CTA***
1992-70 C
(22214)
1992 Oct 22.72
10 days
1992 Nov 1
T-section
plate
82
2.0 long
1.2 wide
0.5 high
1992 Oct 31.4
28.46
88.53
6590
208
215
0.001
291
#
*
-
Strela-3 satellite
Launch and landing at Cape Canaveral (1 woman, 5 men including a Canadian payload specialist).
Cargo bay carried US Microgravity Payload, USMP-1 (not separated) and Canadian experiments, CANEX-2,
extensions of CANEX on STS-41G (see page 807).
** Built by Agenzia Spaziale Italiana (ASI) using drawings and specifications for Lageos 1 (see page 445).
Ejected from Shuttle on 1992 Oct 23.58
*** Canadian Target Assembly ejected from Shuttle on 1992 Oct 31.42.
2004 December 31 – version 1.01
1992-70 continued on page 1106
RAE Table of Earth Satellites
Year of Launch 1992
Name
[Launcher]
Fragments
Cospar ID
[Norad #] Launchsite
Cospar ID
(Revised 2001)
Launchdate
Lifetime + Descent date
[Norad]
Shape and
weight (kg)
Descent date
Size
(m)
Lifetime
Date of
orbital
determination
Orbital
Inclination
(deg)
Nodal
period
(min)
Semi
major axis
(km)
Page 1106
Perigee
height
(km)
Apogee
height
(km)
Orbital
Argument
eccentricity of perigee
(deg)
Lageos 2
IRIS*
1992-70 D
(22196)
1992 Oct 22.72
20 years
Conecylinder
1726 full
250 empty
1.94 long
1.30 to
1.58 dia
1992 Oct 25.6
2001 Dec 20.40
41.21
41.21
153.20
138.57
9489
8871
296
287
5926
4697
0.297
0.249
185
233
Lageos 2
Mage 1S
Apogee stage
1992-70 E
(22197)
1992 Oct 22.72
1 million
years
Conecylinder
400? full
37 empty
1.29 long
0.77 dia
1992 Oct 25.2
2001 Dec 19.80
52.64
52.63
222.39
222.42
12161
12161
5616
5615
5949
5949
0.014
0.014
215
237
D? Lageos 2 Fragment
IRIS fragment
1992-70 F
1992-70 G
[22198]
[22535]
1993 Jan 1 A
70 days?
2001 Dec 21.24
41.14
122.30
8162
288
3279
0.183
72
D
Progress-M 15**
[Soyuz 11A511U2
15000-061]
1992-71 A
(22203)
BAI-LC31
1992 Oct 27.72
103 days
1993 Feb 7
Spherecylinder +
2 panels
7020?
7.9 long?
2.3 dia?
1992 Oct 29.0
51.62
90.38
6674
269
323
0.004
116
D
Progress-M 15
Block I 3rd stage
1992-71 B
(22204)
1992 Oct 27.72
1 day
1992 Oct 28
Cylinder
2500?
7.5 long?
2.6 dia?
1992 Oct 28.9
51.60
88.30
6572
185
203
0.001
62
D
Znamya
Sunreflector
1992-71 C
[22449]
1992 Oct 27.72
101 days
1993 Feb 5
Galaxy 7
[Ariane 4-26]
1992-72 A
(22205)
KOU-ELA2
1992 Oct 28.01
>million
years
Box +
panels
1680 full
1303 empty
Ariane 42P V54
third stage
1992-72 B
(22206)
1992 Oct 28.01
667 days
1994 Aug 26
Cylinder
12100 full
1242 empty
Fragments
1992-72 C-P
12 pieces, 4 have decayed
Cosmos 2218
[Cosmos 11K65M
65078-424]
1992-73 A
(22207)
PLE
1992 Oct 29.45
1200 years
Cylinder
810
2.1 long
2.0 dia
1992 Oct 29.6
2001 Dec 20.85
82.92
82.92
105.00
104.90
7370
7369
968
966
1015
1014
0.003
0.003
276
10
Cosmos 2218
2nd stage
1992-73 B
(22208)
1992 Oct 29.45
600 years
Cylinder
2200?
7.4 long
2.4 dia
1992 Oct 30.4
2001 Dec 19.81
82.92
82.92
104.86
104.75
7363
7362
967
958
1004
1007
0.002
0.003
265
330
* Italian Research Interim Stage
** Progress-M 15 docked with Kvant 1 (-X port) on 1992 Oct 29.80.
2004 December 31 – version 1.01
Ejected from Progress-M 15 after experiments were completed.
1993 Feb 4.66
51.62
92.39
6770
390
393
0.0002
329
3.6 x
3.1 x
2.7
26.5 span
1992
1992
1992
2000
2001
11.7 long
2.6 dia
1992 Nov 5.9
Oct
Nov
Nov
Dec
Dec
29.2
7.1
17.1
2.15
21.28
6.95
0.14
0.15
0.10
0.98
518.52
1435.21
1436.01
1445.23
1444.05
21395
42149
42165
42343
42320
199
35684
35715
35861
35872
29834
35858
35859
36069
36011
0.693
0.002
0.002
0.003
0.002
178
115
86
153
161
7.14
482.56
20394
260
27772
0.675
187
For orbital information see extra pages at the end of the year
RAE Table of Earth Satellites
Year of Launch 1992
Name
[Launcher]
Fragments
Cospar ID
[Norad #] Launchsite
Cospar ID
Shape and
weight (kg)
Descent date
Ekran 20
1992-74 A
[Proton 8K82K
(22210)
372-01/11S861 58L] BAI-LC81L
1992 Oct 30.63
>million
years
Cylinder +
plate
2000?
D
Ekran 20
third stage
1992-74 B
(22211)
1992 Oct 30.63
2 days
1992 Nov 1
Cylinder
6.5 long?
4 dia
1992 Oct 30.8
51.66
D
Ekran 20
4th stage casing
1992-74 C
(22212)
1992 Oct 30.63
1 day
1992 Oct 31
Irregular
-
1992 Oct 30.7
51.66
Ekran 20
Block DM 2
fourth stage
1992-74 D
(22213)
1992 Oct 30.63
>million
years
Cylinder
17300
full
5.5 long
4.0 dia
1992 Oct 30.6
2001 Dec 15.61
1.55
5.21
D
Ekran 20
Ullage motor
1992-74 E
[22215]
1992 Oct 30.63
505 days
1994 Mar 19
Ellipsoid
55
1.0 long
0.6 dia
D
Ekran 20
Ullage motor
1992-74 F
[22215]
1992 Oct 30.63
214 days
1993 Jun 3
Ellipsoid
55
1.0 long
0.6 dia
D
R
Resurs-500*
[Soyuz 11A511U]
1992-75 A
(22217)
PLE-LC16
1992 Nov 15.91
6.87 days
1992 Nov 22.78
Sphere-cone
6300
6.5 long?
2.4 dia
1992 Nov 17.7
1992 Nov 17.9
1992 Nov 22.6
82.57
82.57
82.58
D
Resurs-500
Block I 3rd stage
1992-75 B
(22218)
1992 Nov 15.91
3 days
1992 Nov 18
Cylinder
2500?
7.5 long
2.6 dia
1992 Nov 16.0
D
Resurs-500
engine
1992-75 C
(22234)
1992 Nov 15.91
15 days
1992 Nov 30
Cone
600?
full
1.9 long
1.0 dia
1992 Nov 23.6
D
Fragment
1992-75 D
[22235]
1992 Nov 28
13 days
*
Europe-America-500 Programme.
2004 December 31 – version 1.01
Size
(m)
Lifetime
(Revised 2001)
Launchdate
Lifetime + Descent date
[Norad]
-
Date of
orbital
determination
Orbital
Inclination
(deg)
1992
1992
1992
2001
1.58
1.51
1.47
5.31
Oct
Nov
Nov
Dec
30.6
3.4
22.3
21.62
Page 1107
Nodal
period
(min)
Semi
major axis
(km)
Perigee
height
(km)
Apogee
height
(km)
Orbital
Argument
eccentricity of perigee
(deg)
1428.19
1431.76
1435.80
1436.70
42012
42082
42161
42177
35575
35624
35766
35786
35692
35783
35800
35810
0.001
0.002
0.0004
0.0003
197
130
197
357
88.19
6566
182
194
0.001
316
88.39
6576
192
204
0.001
34
41917
41922
35490
35449
35588
35638
0.001
0.002
339
255
88.74
90.40
89.46
6587
6669
6623
179
222
187
239
360
303
0.005
0.010
0.009
88
191
212
82.59
88.73
6587
181
235
0.004
95
82.58
89.30
6615
182
291
0.008
209
1423.35
1423.70
Recovered in the Pacific Ocean by the Marshal Krylov 320 km SW of Seattle, USA.
RAE Table of Earth Satellites
Year of Launch 1992
Name
[Launcher]
Fragments
Cospar ID
[Norad #] Launchsite
Cospar ID
Launchdate
Lifetime + Descent date
[Norad]
Shape and
weight (kg)
Descent date
Size
(m)
Lifetime
(Revised 2001)
Date of
orbital
determination
Orbital
Inclination
(deg)
Nodal
period
(min)
-
1992 Nov 21.9
2001 Dec 21.90
71.01
71.06
102.00
101.90
10.4 long
3.9 dia
1992 Nov 17.6
2001 Dec 22.54
71.00
71.00
Semi
major axis
(km)
Page 1108
Perigee
height
(km)
Apogee
height
(km)
Orbital
Argument
eccentricity of perigee
(deg)
7230
7227
849
834
855
863
0.0004
0.002
63
18
101.81
101.70
7221
7218
838
828
848
850
0.001
0.001
303
251
Cosmos 2219
[Zenit-2]
1992-76 A
(22219)
BAI-LC45L
1992 Nov 17.33
300 years
6000
Cosmos 2219
rocket
1992-76 B
(22220)
1992 Nov 17.33
200 years
Cylinder
8300
1992-76 C
cap [22221]
1992-76 D
cap [22222]
1992-76 E
cap [22223]
1992-76 F
cap [22224]
1992 Nov 17.33
2001 Dec 20.87
71.04
104.65
7357
842
1114
0.018
1
1992 Nov 17.33
2001 Dec 19.78
70.99
105.18
7382
844
1163
0.022
86
1992 Nov 17.33
2001 Dec 19.64
71.03
104.78
7363
841
1127
0.019
51
1992 Nov 17.33
2001 Dec 21.02
70.98
104.85
7366
844
1130
0.019
76
Cosmos 2219
Separation motor
Cosmos 2219
Separation motor
Cosmos 2219
Separation motor
Cosmos 2219
Separation motor
D
R
Cosmos 2220
[Soyuz 11A511U]
1992-77 A
(22226)
PLE
1992 Nov 20.65
59.1 days
1993 Jan 18.8
Spherecylinder
6700?
7 long?
2.4 dia
1992 Nov 20.9
67.14
89.62
6633
167
342
0.013
93
D
Cosmos 2220
Block I 3rd stage
1992-77 B
(22227)
1992 Nov 20.65
4 days
1992 Nov 24
Cylinder
2500?
7.5 long
2.6 dia
1992 Nov 20.8
67.14
89.57
6630
167
337
0.013
92
D
MSTI*
[Scout G-1 S210C]
1992-78 A
(22229)
VDB-SLC5
1992 Nov 21.57
240 days
1993 Jul 18
Box + vane
180
1.0? x
0.7? x
0.7?
1992 Nov 22.1
96.75
92.37
6766
331
444
0.008
242
D
Altair
Scout 4th stage
1992-78 B
(22230)
1992 Nov 21.57
80 days
1993 Feb 9
Cylinder
24
1.50 long
0.46 dia
1992 Nov 22.3
96.76
92.36
6765
330
444
0.008
242
GPS 2-16 (USA 85)
Navstar
[Delta 7925 #216]
1992-79 A
(22231)
CC-LC17A
1992 Nov 23.0†
1 million
years
Cylinder +
4 vanes
1667 full
844 empty
2.4 long?
1.8 dia?
5.3 span?
1992 Nov 26.4
1992 Dec 27.7
2001 Dec 19.50
54.83
54.85
55.40
714.72
717.97
717.98
26481 19926
26561 20076
26.561 20041
20279
20289
20324
0.007
0.004
0.005
173
298
261
Delta 2
second stage
1992-79 B
(22232)
1992 Nov 23.0†
20 years
Cylinder
6983 full
919 empty
5.88 long
2.44 dia
1992 Nov 25.0
2001 Dec 20.45
21.22
21.21
96.98
95.88
7003
6940
528
493
721
629
0.014
0.001
203
154
GPS 2-16
PAM-D PKM
1992-79 C
(22233)
Cylinder
2154? full
2.29 long
1.5 dia
1992 Nov 24.8
2001 Mar 24.10
34.68
34.48
355.91
89.73
16644
6640
188
134
20344
389
0.606
0.019
195
120
D
*
†
1992 Nov 23.0†
3044 days
2001 Mar 24
Miniature Seeker Technology Integration for SDIO.
Launched at 23:54 UT, 1992 Nov 22
2004 December 31 – version 1.01
RAE Table of Earth Satellites
Year of Launch 1992
Name
[Launcher]
Fragments
Cospar ID
[Norad #] Launchsite
Cospar ID
Launchdate
Lifetime + Descent date
[Norad]
Shape and
weight (kg)
Descent date
Size
(m)
Lifetime
(Revised 2001)
Date of
orbital
determination
Orbital
Inclination
(deg)
Nodal
period
(min)
Semi
major axis
(km)
Page 1109
Perigee
height
(km)
Apogee
height
(km)
Orbital
Argument
eccentricity of perigee
(deg)
Cosmos 2221
[Tsiklon 3]
1992-80 A
(22236)
PLE-LC32
1992 Nov 24.18
60 years
-
-
1992 Nov 25.0
2001 Dec 19.93
82.51
82.51
97.80
97.35
7029
7010
636
619
665
644
0.002
0.002
276
308
Cosmos 2221
3rd stage
1992-80 B
(22237)
1992 Nov 24.18
60 years
Cylinder
2200?
7.4 long
2.4 dia
1992 Nov 25.0
2001 Dec 19.97
82.51
82.51
97.78
97.57
7028
7021
635
629
664
656
0.002
0.002
275
322
Cosmos 2222
[Molniya
8K78M / 2BL]
1992-81 A
(22238)
PLE-LC43/3
1992 Nov 25.51
100 years?
Windmill +
6 vanes
1250?
4.2 long?
1.6 dia
1992 Nov 25.6
1992 Nov 28.5
2001 Dec 20.85
62.88
62.89
67.03
708.15
717.83
718.78
26318
26557
26581
591
594
5029
39288
39763
35375
0.735
0.737
0.571
318
318
288
D
Cosmos 2222
Block I 3rd stage
1992-81 B
(22239)
1992 Nov 25.51
33 days
1992 Dec 28
Cylinder
2500?
7.5 long
2.6 dia
1992 Nov 25.6
62.79
92.31
6766
212
564
0.026
123
D
Cosmos 2222
4th stage casing
1992-81 C
(22240)
1992 Nov 25.51
19 days
1992 Dec 14
Irregular
1992 Nov 25.6
62.80
92.57
6779
181
620
0.032
122
Cosmos 2222
Block L 4th stage
1992-81 D
(22241)
1992 Nov 25.51
100 years?
Cylinder
440 empty
2.0 long
2.0 dia
1992 Nov 25.6
2001 Dec 17.53
62.78
67.44
703.23
707.82
26196
26309
594
4664
39041
35198
0.734
0.580
318
267
D
Cosmos 2222
Ullage motor
1992-81 E
[22242]
1992 Nov 25.51
20 days
1992 Dec 15
Ellipsoid
55
1.0 long
0.6 dia
D
Cosmos 2222 *
Ullage motor
1992-81 F
[22243]
1992 Nov 25.51
4 days
1992 Nov 29
Ellipsoid
55
1.0 long
0.6 dia
D
Fragment
1992-81 G
[22244]
1992 Dec 9
14 days
Gorizont 27
1992-82 A
[Proton 8K82K
(22245)
364-01/11S861 65L] BAI-LC81L
1992 Nov 27.55
>million
years
Cylinder +
dish +
panels
2000?
-
1992 Nov 28.3
2001 Dec 20.97
1.46
5.35
1472.38
1436.03
42874
42164
36469
35770
36523
35800
0.001
0.0004
301
243
D
Gorizont 27
third stage
1992-82 B
(22246)
1992 Nov 27.55
2 days
1992 Nov 29
Cylinder
6.5 long?
4 dia
1992 Nov 27.7
51.65
88.28
6571
190
195
0.0004
1
D
Gorizont 27
4th stage casing
1992-82 C
(22247)
1992 Nov 27.55
1 day
1992 Nov 28
Irregular
-
1992 Nov 27.7
51.64
88.33
6573
181
209
0.002
127
* Fragmented, see extra page 1992-2
2004 December 31 – version 1.01
-
1992-82 continued on page 1110
RAE Table of Earth Satellites
Year of Launch 1992
Name
[Launcher]
Fragments
Cospar ID
[Norad #] Launchsite
Cospar ID
Shape and
weight (kg)
Descent date
Size
(m)
Lifetime
Date of
orbital
determination
Orbital
Inclination
(deg)
1992 Nov 27.55
>million
years
1992 Nov 27.55
230 days
1993 Jul 14
1992 Nov 27.55
3231 days
2001 Oct 2
Cylinder
17300 full
5.5 long
4.0 dia
1992 Nov 30.4
2001 Dec 12.92
1.47
5.47
Ellipsoid
55
1.0 long
0.6 dia
Ellipsoid
55
1.0 long
0.6 dia
2001 Oct 2.57
46.32
-
Gorizont 27
Block DM 2
fourth stage
Gorizont 27
Ullage rocket
1992-82 D
(22248)
D
Gorizont 27
Ullage rocket
1992-82 F
[22250]
D
USA 86
[Titan 404
K-3 (45J-1)]
1992-83 A
(22251)
VDB-SLC4E
1992 Nov 28.90
2746 days
2000 Jun 5
-
Titan 4
second stage
1992-83 B
(22252)
1992 Nov 28.90
Cylinder
Superbird A1
[Ariane 4-27]
1992-84 A
(22253)
KOU-ELA2
1992 Dec 1.95
>million
years
Ariane 42P V55
third stage
1992-84 B
(22254)
Molniya-3 43
[Molniya
8K78M / ML]
D
D
D
D
1992-82 E
[22249]
(Revised 2001)
Launchdate
Lifetime + Descent date
[Norad]
Page 1110
Nodal
period
(min)
Semi
major axis
(km)
Perigee
height
(km)
Apogee
height
(km)
Orbital
Argument
eccentricity of perigee
(deg)
1468.95
1469.00
42807
42806
36358
36375
36501
36480
0.002
0.001
339
220
6655
119
433
0.024
41
90.03
Orbital data not released
No elements available
9.8 long
3 dia
No elements available
Box +
panels
1665 full
1255 empty
3.4 x
2.4 x
2.2
20.3 span
1992
1992
1992
2001
2.2
3.1
12.3
17.40
7.16
2.54
0.09
0.07
635.20
818.20
1435.98
1436.10
24494
28983
42165
42165
237
9427
35759
35771
35994
35782
35814
35802
0.730
0.455
0.001
0.0004
179
180
311
144
1992 Dec 1.95
30 years
Cylinder
12386 full
1242 empty
11.7 long
2.6 dia
1992 Dec 9.2
2001 Dec 21.58
6.97
7.09
630.99
491.03
24385
20618
214
229
35801
28249
0.730
0.679
184
342
1992-85 A
(22255)
PLE-LC43/3
1992 Dec 2.09
10 years?
Windmill +
6 vanes
1000?
3.4 long
1.6 dia
1992 Dec 3.1
1992 Dec 8.5
2001 Dec 17.22
62.83
62.83
64.23
701.22
717.40
717.57
26146
26546
26550
421
413
1041
39114
39923
39302
0.740
0.744
0.721
280
280
266
Molniya-3 43
Block I 3rd stage
1992-85 B
(22256)
1992 Dec 2.09
12 days
1992 Dec 14
Cylinder
2500?
7.5 long
2.6 dia
1992 Dec 3.1
62.79
90.39
6672
208
380
0.013
136
Molniya-3 43
4th stage casing
1992-85 C
(22257)
1992 Dec 2.09
9 days
1992 Dec 11
Irregular
-
1992 Dec 2.4
62.82
90.86
6695
180
453
0.020
126
Molniya-3 43
Block L 4th stage
1992-85 D
(22258)
1992 Dec 2.09
10 years
Cylinder
440
empty
2.0 long
2.0 dia
1992 Dec 4.1
2001 Dec 19.97
62.83
63.85
697.90
697.42
36063
26051
422
1000
38948
38345
0.739
0.717
280
264
Molniya-3 43 *
Ullage rocket
1992-85 E
[22262]
1992 Dec 2.09
13 days
1992 Dec 15
* Originally listed on page 1111.
2004 December 31 – version 1.01
Orbital data not released
Dec
Dec
Dec
Dec
RAE Table of Earth Satellites
Year of Launch 1992
Name
[Launcher]
Fragments
Cospar ID
[Norad #] Launchsite
Cospar ID
(Revised 2001)
Launchdate
Lifetime + Descent date
[Norad]
Shape and
weight (kg)
Descent date
Size
(m)
Lifetime
Date of
orbital
determination
Orbital
Inclination
(deg)
1992-86 A
(22259)
CC-LC39A
1992 Dec 2.56
7.30 days
1992 Dec 9.86
Cylinder +
delta wing
87564
empty
37.1 long
17.4 high
23.8 span
1992 Dec 2.8
1992 Dec 4.4
1992 Dec 8.0
57.00
57.00
56.99
DoD-1**
(USA 89)
1992-86 B
[22518]
1992 Dec 2.56
manoeuvrable
-
1992 Dec 14.6
56.98
DoD-1 PKM
1992-86 C
1992 Dec 2.56
[22519]
1992- 86 D-F 3 pieces
2001 Dec 20.77
56.91
D STS 53*
5M (Discovery F15)
R [Shuttle]
Fragments
700
Nodal
period
(min)
Page 1111
Perigee
height
(km)
Apogee
height
(km)
Orbital
Argument
eccentricity of perigee
(deg)
369
317
317
379
331
322
0.001
0.001
0.0003
304
265
233
Ejected from Shuttle 1992 Dec 2.80
91.96
6750
372
373
0.0001
355
92.00
90.98
90.88
166.50
Semi
major axis
(km)
6752
6702
6698
10039
328
6993
0.332
90
For orbital information see extra pages at the end of the year
D
Cosmos 2223
[Soyuz 11A511U2]
1992-87 A
(22260)
BAI
1992 Dec 9.48
372.1 days
1993 Dec 16.6
Spherecylinder
6700?
7 long?
2.4 dia
1992 Dec 10.8
64.66
89.84
6644
240
292
0.004
76
D
Cosmos 2223
rocket
1992-87 B
(22261)
1992 Dec 9.48
3 days
1992 Dec 12
Cylinder
2500?
7.5 long
2.6 dia
1992 Dec 10.0
64.67
89.01
6603
178
273
0.007
65
D
Fragment
1992-87 C
[22929]
1993 Dec 19
375 days
1993 Dec 17.00
64.40
90.59
6682
227
380
0.011
56
42308
42173
42134
35882
35780
35749
35978
35810
35761
0.001
0.0004
0.0001
175
1
325
Cosmos 2224***
1992-88 A
[Proton 8K82K
(22269)
357-02/11S861 64L] BAI-LC200L
1992 Dec 17.54
>million
years
-
-
1992 Dec 21.3
1999 Jun 8.97
2001 Dec 20.66
2.29
2.51
4.37
D
Cosmos 2224
third stage
1992-88 B
(22270)
1992 Dec 17.54
2 days
1992 Dec 19
Cylinder
6.5 long?
4 dia
1992 Dec 17.8
51.63
88.22
6568
188
191
0.0003
301
D
Cosmos 2224
4th stage casing
1992-88 C
(22271)
1992 Dec 17.54
1 day
1992 Dec 18
Irregular
-
1992 Dec 17.8
51.62
88.12
6563
179
190
0.001
83
Cosmos 2224
Block DM2
fourth stage
Cosmos 2224 #
Ullage motor
1992-88 D
(22272)
Cylinder
17300
full
Ellipsoid
55
5.5 long
4.0 dia
1992 Dec 21.3
2001 Dec 21.49
2.31
4.35
1439.27
1438.77
42229
42217
35812
35794
35889
35883
0.001
0.001
1
270
1.0 long
0.6 dia
2001 Dec 19.30
47.46
594.45
23419
402
33680
0.710
191
Cosmos 2224
Ullage motor
1992-88 F
[22274]
1992 Dec 17.54
>million
years
1992 Dec 17.54
4210 days
2004 Jun 27
1992 Dec 17.54
llipsoid
55
1.0 long
0.6 dia
2001 Dec 19.31
46.48
456.58
19642
205
26321
0.665
132
D
1992-88 E
[22273]
1443.30
1436.54
1434.52
# 1992-88 E fragmented 2000 Feb 29 due to a yet unknown cause. No objects are catalogued.
* Launched from Cape Canaveral; landed at Edwards AFB, California. Last dedicated DoD Shuttle mission.
** Orbit derived from visual observations. Manoeuvred to a much different orbit, in the manner of USA 40 (see page 992), sometime on or before 1992 Dec 16.
*** First to be announced at launch as being in the Prognoz remote sensing series.
2004 December 31 – version 1.01
RAE Table of Earth Satellites
Year of Launch 1992
Name
[Launcher]
Fragments
Cospar ID
[Norad #] Launchsite
Cospar ID
(Revised 2001)
Launchdate
Lifetime + Descent date
[Norad]
Shape and
weight (kg)
Descent date
Size
(m)
Lifetime
Date of
orbital
determination
Orbital
Inclination
(deg)
Nodal
period
(min)
Page 1112
Semi
major axis
(km)
Perigee
height
(km)
Apogee
height
(km)
Orbital
Argument
eccentricity of perigee
(deg)
26717
26560
26563
20128
20039
19947
20551
20325
20421
0.008
0.005
0.009
308
259
255
7051
7028
611
595
735
703
0.009
0.008
208
26
GPS 2-17 (USA 87)
(Navstar 29)
[Delta 7925 #217]
1992-89 A
(22275)
CC-LC17B
1992 Dec 18.93
1 million
years
Cylinder +
4 vanes
1667 full
844 empty
5.3 span?
2.4 long?
1.8 dia?
1992 Dec 20.8
1992 Dec 31.3
2001 Dec 19.39
54.75
54.75
55.39
724.33
717.95
718.07
Delta 2
second stage
1992-89 B
(22276)
1992 Dec 18.93
30 years
Cylinder
6983 full
919 empty
5.88 long
2.44 dia
1992 Dec 21.8
2001 Dec 19.48
20.29
20.29
97.98
97.72
GPS 2-17
PAM-D PKM
1992-89 C
(22277)
1992 Dec 18.93
10 years
Cylinder
2154?
full
2.29 long
1.5 dia
1992 Dec 20.5
2001 Dec 22.45
34.95
34.88
356.85
158.75
16673
9712
184
232
20406
6434
0.606
0.319
194
130
PAM-D fragment
1992-89 D
[22849]
2001 Dec 19.73
35.01
227.58
12348
222
11716
0.465
227
D
Optus B2 *
+ CZ-2E 3rd stage
[CZ-2E #3]
1992-90 A
(22278)
XI-LC2
1992 Dec 21.47
920 days
1995 Jun 29
Sphere-cone
+ box?
10600?
5 long?
2.3 to
1.6 dia?
1992 Dec 31.6
28.15
96.88
6997
208
1029
0.059
234
D
CZ-2E second
stage
1992-90 B
(22279)
1992 Dec 21.47
181 days
1993 Jun 19
Cylinder
15.52 long
3.35 dia
1992 Dec 31.8
28.15
96.68
0.057
236
D
Cosmos 2225
[Soyuz 11A511U2]
1992-91 A
(22280)
BAI
1992 Dec 22.50
58 days
1993 Feb 18
Spherecylinder
6700?
7 long?
2.4 dia
1992 Dec 24.6
64.90
89.72
6638
214
306
0.007
70
D
Cosmos 2225
Block I 3rd stage
1992-91 B
(22281)
1992 Dec 22.50
4 days
1992 Dec 26
Cylinder
2500?
7.5 long
2.6 dia
1992 Dec 22.7
64.92
89.27
6616
170
306
0.010
66
D
Fragments
1992-91 C-G
5 pieces, all have decayed
Cosmos 2226**
(Mussan)
[Tsiklon 3]
1992-92 A
(22282)
PLE-LC32
1992 Dec 22.52
10000 years
-
L
Cosmos 2226
rocket
1992-92 B
(22283)
1992 Dec 22.52
10000 years
Cylinder
2200?
208
1010
For orbital information see extra pages at the end of the year
-
7.4 long
2.4 dia
1992 Dec 22.8
2001 Dec 19.69
73.63
73.62
116.07
116.02
7880
7880
1478
1478
1526
1525
0.003
0.003
277
250
1992 Dec 22.8
2001 Dec 19.93
73.63
73.62
116.03
115.35
7878
7850
1478
1426
1523
1517
0.003
0.006
280
163
* Domestic satellite for Optus Communications, Australia, originally known as Aussat B2.
** Probably also known as GEO-IK4.
2004 December 31 – version 1.01
6987
Probably still attached to Star 63F perigee kick motor.
RAE Table of Earth Satellites
Year of Launch 1992
Name
[Launcher]
Fragments
Cospar ID
[Norad #] Launchsite
Cospar ID
Launchdate
Lifetime + Descent date
[Norad]
Shape and
weight (kg)
Descent date
Size
(m)
Lifetime
(Revised 2001)
Date of
orbital
determination
Orbital
Inclination
(deg)
Nodal
period
(min)
Semi
major axis
(km)
Page 1113
Perigee
height
(km)
Apogee
height
(km)
Orbital
Argument
eccentricity of perigee
(deg)
Cosmos 2227
[Zenit-2]
1992-93 A
(22284)
BAI-LC45L
1992 Dec 25.25
300 years
-
-
1992 Dec 30.1
2001 Dec 20.07
71.03
70.97
101.99
101.93
7230
7229
849
845
854
855
0.0004
0.0007
56
156
Cosmos 2227
Zenit 2nd stage
1992-93 B
(22285)
1992 Dec 25.25
disintegrated
1992 Dec 26
Cylinder
8300
10.4 long
3.9 dia
1992 Dec 29.7
2001 Dec 20.80
71.02
71.02
101.88
101.80
7224
7223
845
841
848
846
0.0002
0.0003
20
124
Separ.
Separ.
Separ.
Separ.
1992-93
1992-93
1992-93
1992-93
[22290]
[22291]
[22292]
[22293]
2001
2001
2001
2001
71.05
71.01
71.01
71.06
104.83
105.05
105.15
104.87
7365
7375
7380
7367
842
842
844
843
1131
1151
1159
1133
0.020
0.021
0.021
0.020
101
116
147
75
Motor
Motor
Motor
Motor
cap
cap
cap
cap
Fragments
E
F
G
H
1992-93 C,D,J-JP
228 pieces, 521 have decayed
Dec
Dec
Dec
Dec
19.91
19.98
21.42
20.04
For orbital information see extra pages at the end of the year
Cosmos 2228
[Tsiklon 3]
1992-94 A
(22286)
PLE-LC32
1992 Dec 25.84
60 years
-
-
1992 Dec 27.9
2001 Dec 22.36
82.53
82.52
97.81
97.35
7029
7011
633
613
669
650
0.003
0.003
288
60
Cosmos 2228
3rd stage
1992-94 B
(22287)
1992 Dec 25.84
60 years
Cylinder
2200?
7.4 long
2.4 dia
1992 Dec 27.1
2001 Dec 19.87
82.53
82.52
97.79
97.58
7028
7021
632
623
668
662
0.003
0.003
294
78
Fragment
1992-94 C
[23104]
1994 May 11.50
82.53
97.72
7028
630
670
0.003
105
D
B
R
Cosmos 2229*
(Bion 10)
[Soyuz 11A511U]
1992-95 A
(22300)
PLE-LC43/3
1992 Dec 29.56
11.62 days
1993 Jan 10.18
Sphere6300?
5.9 long
1992 Dec 30.2
62.81
90.44
6674
218
375
0.012
111
D
Cosmos 2229
3rd stage
1992-95 B
(22301)
1992 Dec 29.56
18 days
1993 Jan 16
Cylinder
2500?
7.5 long
2.6 dia
1992 Dec 30.1
62.79
90.35
6670
217
366
0.011
110
D
Cosmos 2229
Capsule
1992-95 C
[22302]
1992 Dec 29.56
44 days
1993 Feb 11
D
Fragments
1992-95 D-G
4 pieces all have decayed
*
Biological satellite: carries 2 monkeys, rats, fish, amphibians and other biological organisms.
2004 December 31 – version 1.01
For orbital information see extra pages at the end of the year
RAE Table of Earth Satellites
Year of Launch 1992
Cospar ID
[Norad number]
Descent date
Lifetime
Date of
orbital determination
Determination
(Revised 2001)
Orbital
Inclination
(deg)
Nodal
period
(min)
Semi
major axis
(km)
Extra Page 1992 - 1
Perigee
height
(km)
Apogee
height
(km)
Orbital
Argument
eccentricity of perigee
(deg)
Text in box is from "History of on-orbit satellite fragmentations", 12th edition, 31 July 2001 and 13th edition, May 2004.
Orbital Debris Program Office, Johnson Space Centre, NASA, Houston, TX 77058.
Ariane-4 22 (V50) 3rd stage fragments, 12 pieces; all in orbit
Although analysis indicates that 92-021 C fragmented around 21 April 1993, the event was not recognized until eight pieces were catalogued during the
period from 30 August 1994 to 2 September 1994. Naval Space Command reported that the eight pieces were discovered during the period from July 1993 to
July 1994.
This refers to objects G-Q; although there are nine pieces, but N was re-assigned.
1992-21 E
[22850]
2001 Dec 19.95
3.33
640.67
24618 949
35529 0.702
159
1992-21 F
[22851]
2001 Dec 22.23
3.75
323.58
15613 171
18298 0.580
27
1992-21 G
[23237]
2001 Dec 20.74
3.19
640.30
24609 939
35520 0.703
162
1992-21 H
[23238]
2001 Dec 11.87
3.29
641.67
24643 985
35545 0.701
117
1992-21 J
[23239]
2001 Dec 20.91
3.23
643.40
24688 1029
35590 0.700
62
1992-21 K
[23240]
2001 Dec 20.62
3.17
643.92
24701 1045
35600 0.699
43
1992-21 L
[23241]
2001 Dec 20.69
3.18
641.48
24639 936
35584 0.703
154
1992-21 M
[23242]
2001 Dec 20.63
3.28
641.90
24649 984
35558 0.701
322
1992-21 N
[R23243]
2000 Jan 19.92
3.16
667.52
25301 634
37211 0.723
147
Re-assigned to 1989-27 C
1992-21 P
[23244]
2001 Dec 18.08
4.42
649.87
24853 1372
35577 0.688
277
1992-21 Q
[23245]
2001 Dec 17.55
3.26
642.47
24664 980
35592 0.702
75
1992-21 R
[26790]
2001 Aug 3.48
3.78
645.05
24730 1110
35593 0.697
307
Ariane 44L 3rd stage fragments; 4 pieces, all have decayed.
This event in 2002 Feb marks the sixth known fragmentation of an Ariane 4 third stage. The last three vehicles involved in such events (1988-109C, 1991-075C, and
1992-041C) had been in orbit 9-10 years at the time of their respective break-ups. All flights were conducted prior to the implementation of passivation measures
for Ariane GTO missions in September 1993. No Ariane launch vehicle launched since that time is known to have experienced an on-orbit fragmentation. At least 11
fragments were tracked.
D 1992-41 E
[27484]
2003 Apr 27
3944 days
2003 Apr 23.23
6.91
134.87
8712
125
4541
0.253
274
D 1992-41 F
[27485]
2003 Mar 19
3905 days
D 1992-41 G
[27486]
2003 Jul 4
4012 days
D 1992-41 H
[27487]
2003 Nov 10
4141 days
Cosmos 2204-2206 ullage motor, 1992-47 H
Parent satellite was one of two small engine units which are routinely released after the first burn of the Proton fourth stage. The nature of these
objects was identified by Dr. Boris V. Cherniatiev, Deputy Constructor for the Energiya NPO and Mr. Nicholas Johnson of Kaman Sciences, in October, 1992.
The cause of this fragmentation, which occurred prior to 1994 Nov 8 08:24 UT, appears to be related to the residual hypergolic propellants on board and
failure of the membrane separating the fuel and oxidizer. NAVSPASUR observed 32 objects which were associated with this breakup on 8 Nov 94, 36 objects
on 9 Nov and 31 objects on 10 Nov. This was the tenth in a series of fragmentations of this object type.
None of these fragments were catalogued. Objects in orbit of 500 by 19000 km.
Parent object decayed 2001 Dec 19, 3064 days
Two objects have been catalogued, J in period 1995 Jul 13-20; K in period 1997 Sep 4-19 (see main section).
Cosmos 2207 fragments, 4 pieces, all have decayed
D 1992-48 D
[22082]
1992 Aug 21
D 1992-48 E
[22083]
1992 Aug 18
D 1992-48 F
[22084]
1992 Aug 29
D 1992-48 G
[22085]
1992 Aug 21
2004 December 31 – version 1.01
21
18
29
21
days
days
days
days
RAE Table of Earth Satellites
Year of Launch 1992
Cospar ID
[Norad number]
Descent date
Lifetime
FSW-1 4 fragments, 7 pieces, all have decayed
D 1992-64 D
[22164]
1992 Oct 9
D 1992-64 E
[22165]
1992 Oct 8
D 1992-64 F
[22166]
1992 Oct 9
D 1992-64 G
[22167]
1992 Oct 8
D 1992-64 H
[22168]
1992 Oct 10
D 1992-64 J
[22169]
1992 Oct 9
D 1992-64 K
[22170]
1992 Oct 9
3
2
3
2
4
3
3
Foton 5 fragments, 3 pieces, all have decayed
D 1992-65 D
[22200]
1992 Oct 31
D 1992-65 E
[22201]
1992 Oct 30
D 1992-65 F
[22202]
1992 Nov 3
23 days
22 days
26 days
(Revised 2001)
Date of
orbital determination
Determination
Orbital
Inclination
(deg)
Nodal
period
(min)
2001 Dec 20.63
2001 Dec 6.70
7.20
6.72
452.88
456.20
2001
2001
2000
2001
2001
2001
2004
2004
2004
6.73
6.95
6.95
9.15
7.64
9.55
6.43
8.14
7.79
373.60
96.90
97.22
494.55
497.13
497.43
444.32
496.47
493.68
Semi
major axis
(km)
Extra Page 1992 - 2
Perigee
height
(km)
Apogee
height
(km)
Orbital
Argument
eccentricity of perigee
(deg)
19535
19631
308
537
26005
25967
0.658
0.648
76
225
17183
6989
7004
20716
20788
20796
19288
20770
20692
431
158
217
894
1005
1005
460
987
898
21179
1063
1033
27780
27813
27830
25359
27795
27728
0.604
0.065
0.058
0.649
0.645
0.645
0.645
0.645
0.648
193
358
22
114
58
186
174
275
155
days
days
days
days
days
days
days
Ariane-4 26 3rd stage fragments; 12 pieces, 4 have decayed
1992-72 C
[22670]
1992-72 D
[23301]
D 1992-72 E
[25150]
1998 Aug 8
2110 days
D 1992-72 F
[25151]
2004 May 25
4227 days
D 1992-72 G
[25734]
2001 Mar 27
3072 days
D 1992-72 H
[26413]
2000 Sep 24
2888 days
1992-72 J
[26741]
1992-72 K
[26850]
1992-72 L
[26981]
1992-72 M
[27685]
1992-72 N
[28279]
1992-72 P
[28280]
Dec
Mar
Sep
Dec
Dec
Jul
Dec
Oct
Dec
21.75
24.87
17.43
19.25
20.40
01.09
31.73
14.16
31.76
Gorizont 27 ullage motor fragments; 1992-82 F.
This eventoccurred 2001 Jul 14 around 18:00 UT and marks the 25th known breakup of a Proton Block DM SOZ ullage motor since 1984. Due to the moderate
eccentricity and altitude of the orbits, the debris were difficult for the US Space Surveillance Network to track. This ullage motor was launched before
implementation of breakup preventive measures. No debris were catalogued from this break-up.
DoD-1 fragments; 3 pieces
1992- 86 D
[24865]
1992- 86 E
[24867]
1992- 86 F
[25608]
No TLE found
No TLE found
No TLE found
Cosmos 2225 fragments, 5 pieces, all have decayed
Spacecraft was destroyed 18 Feb 1993 at 18:56 UT near 55N 157E with a planned detonation. Fourth fragmentation of the Cosmos 2031 subclass. Early
elements on only 10 objects (including the parent) available; Flyingdales observed 21 objects soon after the event.
D 1992-91 C
[22520]
1993 Feb 23
63 days
D 1992-91 D
[22525]
1993 Feb 25
65 days
D 1992-91 E
[22526]
1993 Feb 22
62 days
D 1992-91 F
[22527]
1993 Feb 27
67 days
D 1992-91 G
[22529]
1993 Feb 24
64 days
2004 December 31 – version 1.01
RAE Table of Earth Satellites
Year of Launch 1992
Cospar ID
[Norad number]
Descent date
Lifetime
Date of
orbital determination
Determination
(Revised 2001)
Orbital
Inclination
(deg)
Nodal
period
(min)
Semi
major axis
(km)
Extra Page 1992 - 3
Perigee
height
(km)
Apogee
height
(km)
Orbital
Argument
eccentricity of perigee
(deg)
Cosmos 2227 Zenit 2nd stage fragments; 228 pieces, 52 have decayed.
Fragments E-H are the Satellite ejection units.
Four separate events were reported by NAVSPASUR. The first observed event was accompanied by an initial 18 objects, but could not be correlated with the
rocket body element set. The rocket body was the closest object to the blast point. The second event followed 15 hours later with 96 objects. The third
event followed the second by less then 20 minutes and was based upon 51 pieces. 3 objects accompanied the fourth event.
#1 26 Dec 1992 at 07:38 UT near 63N 60E ; #2 26 Dec 1992 at 22:49 UT near 44N 168E; #3 26 Dec 1992 at 23:10 UT near 52N 63E; #4 30 Dec 1992 at 09:03 UT
near 22S 172E. On 24 April 1995 object 22366, 1992-093 BF, fragmented liberating 1 associated piece.
D
D
D
D
1992-93
1992-93
1992-93
1992-93
1992-93
1992-93
1992-93
1992-93
1992-93
1992-93
1992-93
1992-93
1992-93
1992-93
1992-93
1992-93
1992-93
1992-93
1992-93
1992-93
1992-93
1992-93
1992-93
1992-93
1992-93
1992-93
1992-93
1992-93
1992-93
1992-93
1992-93
1992-93
1992-93
1992-93
1992-93
1992-93
1992-93
1992-93
1992-93
1992-93
1992-93
C
D
J
K
L
M
N
P
Q
R
S
T
U
V
W
X
Y
Z
AA
AB
AC
AD
AE
AF
AG
AH
AJ
AK
AL
AM
AN
AP
AQ
AR
AS
AT
AU
AV
AW
AX
AY
[22288]
[22289]
[22294]
[22295]
[22296]
[22297]
[22298]
[22326]
[22327]
[22328]
[22329]
[22330]
[22331]
[22332]
[22333]
[22334]
[22335]
[22336]
[22337]
[22338]
[22339]
[22340]
[22341]
[22342]
[22343]
[22344]
[22345]
[22346]
[22347]
[22348]
[22349]
[22350]
[22351]
[22352]
[22353]
[22354]
[22355]
[22356]
[22357]
[22358]
[22359]
2004 December 31 – version 1.01
1999 Oct 1
2471 days
1999 Dec 11
2542 days
2004 Jun 26
2000 Jan 23
4201 days
2951 days
1999
2001
2001
2001
2001
2001
2001
2001
2001
2001
2001
2001
2001
2001
2001
1999
2001
2001
2001
2001
2001
2001
2001
2001
2001
2001
2001
2000
2001
2001
2001
2001
2001
2001
2001
2001
2001
2001
2001
2001
2001
Oct
Dec
Dec
Dec
Dec
Dec
Dec
Dec
Dec
Dec
Dec
Dec
Dec
Dec
Dec
Dec
Dec
Dec
Dec
Dec
Dec
Dec
Dec
Dec
Dec
Dec
Dec
Jan
Dec
Dec
Dec
Dec
Dec
Dec
Dec
Dec
Dec
Dec
Dec
Dec
Dec
1.08
21.37
20.86
20.32
20.24
20.34
21.11
21.37
21.13
20.19
20.76
20.44
20.32
21.71
20.30
10.82
15.52
16.54
15.20
15.46
14.89
15.62
14.74
15.63
16.50
14.47
15.19
23.36
16.22
15.40
15.69
14.35
16.09
15.02
15.18
16.57
16.47
15.41
15.60
15.19
15.88
71.00
70.83
71.05
71.00
70.88
70.95
70.73
70.66
71.13
70.52
70.91
70.41
70.92
70.57
71.00
70.58
71.17
71.13
71.28
70.62
70.81
70.87
70.75
70.70
70.96
71.10
70.56
70.77
70.84
71.26
70.82
70.91
70.91
70.89
70.97
71.14
71.24
70.70
70.88
71.22
70.75
90.75
100.75
102.15
102.50
102.00
102.68
93.57
104.00
99.00
100.35
99.43
102.77
102.58
101.43
100.03
90.30
103.55
103.58
104.08
99.48
100.55
103.33
103.70
103.63
102.65
103.20
99.65
89.52
104.50
102.75
104.53
102.53
102.97
102.85
102.92
103.52
100.20
102.22
99.08
104.07
104.25
6690
7172
7239
7256
7232
7264
6828
7326
7089
7154
7110
7268
7259
7205
7138
6668
7305
7311
7330
7112
7163
7294
7312
7309
7263
7289
7121
6629
7350
7267
7351
7257
7278
7272
7275
7303
7146
7242
7093
7330
7338
310
749
789
805
785
808
431
830
617
753
652
800
823
787
665
269
834
841
840
656
689
841
837
841
807
820
697
226
814
808
833
828
818
837
800
818
750
804
634
842
823
313
838
931
950
921
962
467
1065
804
798
811
979
938
866
855
310
1018
1024
1062
811
879
990
1030
1019
961
1000
787
275
1128
969
1111
928
981
950
993
1032
785
923
795
1060
1096
0.0002
0.006
0.010
0.010
0.010
0.011
0.003
0.016
0.013
0.003
0.011
0.012
0.008
0.005
0.013
0.003
0.013
0.012
0.015
0.011
0.013
0.010
0.013
0.012
0.011
0.012
0.006
0.004
0.021
0.011
0.019
0.007
0.011
0.008
0.013
0.015
0.002
0.008
0.011
0.015
0.019
122
1
58
150
49
216
63
203
270
324
88
253
214
83
48
173
314
344
277
347
212
358
109
134
229
346
49
346
239
120
135
11
287
287
263
187
356
64
207
314
167
RAE Table of Earth Satellites
Year of Launch 1992
Cospar ID
D
[Norad number]
1992-93 AZ
[22360]
1992-93 BA
[22361]
1992-93 BB
[22362]
1992-93 BC
[22363]
1992-93 BD
[22364]
D 1992-93 BE
[22365]
1992-93 BF
[22366]
1992-93 BG
[22367]
1992-93 BH
[22368]
1992-93 BJ
[22369]
1992-93 BK
[22370]
1992-93 BL
[22371]
1992-93 BM
[22372]
D 1992-93 BN
[22373]
1992-93 BP
[22374]
1992-93 BQ
[22375]
1992-93 BR
[22376]
1992-93 BS
[22377]
1992-93 BT
[22378]
1992-93 BU
[22379]
D 1992-93 BV
[22380]
1992-93 BW
[22381]
1992-93 BX
[22382]
1992-93 BY
[22383]
D 1992-93 BZ
[22384]
D 1992-93 CA
[22385]
D 1992-93 CB
[22386]
1992-93 CC
[22387]
1992-93 CD
[22388]
D 1992-93 CE
[22389]
1992-93 CF
[22390]
1992-93 CG
[22391]
1992-93 CH
[22392]
1992-93 CJ
[22393]
1992-93 CK
[22394]
1992-93 CL
[22395]
1992-93 CM
[22396]
1992-93 CN
[22397]
1992-93 CP
[22398]
D 1992-93 CQ
[22399]
1992-93 CR
[22400]
D 1992-93 CS
[22401]
D 1992-93 CT
[22402]
1992-93 CU
[22403]
1992-93 CV
[22404]
1992-93 CW
[22405]
1992-93 CX
[22406]
1992-93 CY
[22407]
1992-93 CZ
[22408]
1992-93 DA
[22409]
2004 December 31 – version 1.01
Descent date
Lifetime
1999 Nov 20
2521 days
1999 Dec 9
2540 days
2000 Nov 29
2896 days
2000 Dec 9
2540 days
2000 Oct 29
2001 Oct 29
1999 Nov 15
2865 days
3230 days
2516 days
2003 Oct 27
3958 days
2003 Oct 26
3957 days
2003 Jun 29
2000 Jul 9
3838 days
2753 days
(Revised 2001)
Date of
orbital determination
Determination
Orbital
Inclination
(deg)
1999
2001
2001
2001
2001
1999
2001
2001
2001
2001
2001
2001
2001
2000
2001
2001
2001
2001
2001
2001
2000
2001
2001
2001
2000
2001
1999
2001
2001
2001
2001
2001
2001
2001
2001
2001
2001
2001
2001
2001
2001
2001
2000
2001
2001
2001
2001
2001
2001
2001
70.77
70.76
70.90
71.03
71.10
71.10
71.12
70.90
71.25
70.88
70.98
71.16
71.09
70.34
70.79
70.81
70.93
71.10
71.26
70.70
70.60
70.53
70.86
70.69
70.63
70.77
70.79
70.89
70.95
71.15
71.17
71.35
70.90
71.13
71.28
71.16
70.67
70.81
70.95
70.98
71.24
71.12
70.59
70.89
71.06
71.03
70.75
70.86
71.09
71.14
Nov
Dec
Dec
Dec
Dec
Dec
Dec
Dec
Dec
Dec
Dec
Dec
Dec
Nov
Dec
Dec
Dec
Dec
Dec
Dec
Dec
Dec
Dec
Dec
Oct
Oct
Nov
Dec
Dec
Dec
Dec
Dec
Dec
Dec
Dec
Dec
Dec
Dec
Dec
Dec
Dec
Dec
Jul
Dec
Dec
Dec
Dec
Dec
Dec
Dec
20.07
15.55
16.41
15.89
15.47
8.62
16.53
14.84
15.08
16.15
14.47
15.88
16.35
29.25
16.06
14.87
15.22
16.17
16.15
16.43
9.86
15.53
15.90
16.50
29.81
28.05
14.56
15.20
16.27
16.53
15.74
15.53
14.50
14.90
16.88
16.91
16.84
16.94
17.21
16.93
16.76
16.95
8.22
16.49
17.16
17.04
16.90
17.59
16.83
17.18
Nodal
period
(min)
89.59
104.60
104.88
103.63
98.32
88.42
102.92
104.20
99.78
103.32
102.75
103.50
94.27
91.08
104.43
102.88
102.20
102.58
96.87
103.03
88.43
101.67
104.20
101.93
90.08
91.77
88.58
103.15
102.98
97.35
102.93
100.75
98.95
103.18
102.90
102.95
101.07
101.90
103.02
97.62
104.00
97.25
90.78
102.95
99.02
100.23
104.45
104.43
103.18
99.42
Semi
major axis
(km)
6652
7354
7368
7309
7057
6575
7275
7336
7126
7294
7268
7302
6861
6706
7347
7274
7241
7259
6987
7281
6575
7216
7336
7229
6657
6739
6583
7286
7278
7010
7276
7173
7087
7288
7274
7277
7187
7227
7280
7023
7326
7005
6691
7277
7090
7148
7347
7347
7288
7109
Extra Page 1992 - 4
Perigee
height
(km)
Apogee
height
(km)
Orbital
Argument
eccentricity of perigee
(deg)
261
834
825
819
616
187
777
818
657
841
804
839
461
313
826
830
808
836
556
834
187
790
830
781
264
352
196
818
807
568
837
736
612
809
833
810
785
815
808
584
827
560
299
832
619
676
836
832
805
629
286
1118
1153
1041
740
205
1015
1096
838
989
974
1008
504
341
1110
960
917
925
661
970
206
884
1084
919
293
369
213
987
992
696
957
852
805
1010
958
986
833
882
994
705
1068
694
326
964
805
863
1101
1105
1013
832
0.002
0.019
0.022
0.015
0.009
0.001
0.016
0.019
0.013
0.010
0.012
0.012
0.003
0.002
0.019
0.009
0.007
0.006
0.007
0.009
0.001
0.007
0.017
0.010
0.002
0.001
0.001
0.012
0.013
0.009
0.008
0.008
0.014
0.014
0.009
0.012
0.003
0.005
0.013
0.009
0.016
0.010
0.002
0.009
0.013
0.013
0.018
0.019
0.014
0.014
175
174
247
270
43
239
205
183
224
350
220
301
150
179
156
97
227
232
158
83
155
118
88
104
346
184
60
336
291
217
228
321
219
191
163
285
334
299
275
339
285
220
260
321
324
310
169
103
212
289
RAE Table of Earth Satellites
Year of Launch 1992
Cospar ID
[Norad number]
1992-93 DB
[22410]
1992-93 DC
[22411]
D 1992-93 DD
[22412]
D 1992-93 DE
[22413]
1992-93 DF
[22414]
1992-93 DG
[22415]
1992-93 DH
[22416]
1992-93 DJ
[22417]
1992-93 DK
[22418]
1992-93 DL
[22419]
1992-93 DM
[22420]
1992-93 DN
[22421]
1992-93 DP
[22422]
1992-93 DQ
[22423]
D 1992-93 DR
[22424]
1992-93 DS
[22425]
1992-93 DT
[22426]
1992-93 DU
[22427]
D 1992-93 DV
[22428]
1992-93 DW
[22429]
1992-93 DX
[22430]
1992-93 DY
[22431]
1992-93 DZ
[22432]
1992-93 EA
[22433]
D 1992-93 EB
[22434]
1992-93 EC
[22435]
1992-93 ED
[22436]
1992-93 EE
[22437]
1992-93 EF
[22438]
D 1992-93 EG
[22439]
D 1992-93 EH
[22440]
1992-93 EJ
[22441]
1992-93 EK
[22442]
1992-93 EL
[22443]
1992-93 EM
[22444]
1992-93 EN
[22445]
D 1992-93 EP
[22450]
1992-93 EQ
[22451]
D 1992-93 ER
[22452]
1992-93 ES
[22453]
1992-93 ET
[22454]
1992-93 EU
[22455]
1992-93 EV
[22456]
D 1992-93 EW
[22457]
1992-93 EX
[22458]
1992-93 EY
[22459]
D 1992-93 EZ
[22460]
D 1992-93 FA
[22461]
1992-93 FB
[22462]
1992-93 FC
[22463]
2004 December 31 – version 1.01
Descent date
Lifetime
2000 Apr 24
2003 Jun 28
2677 days
3837 days
2001 Jun 21
3100 days
1999 Mar 31
2287 days
1999 Nov 16
2517 days
1998 Dec 13
1998 Feb 24
2179 days
1887 days
1997 Sep 17
1727 days
2001 Jan 21
2949 days
2000 Apr 1
3019 days
1993 Jun 24
1996 Jul 24
181 days
1307 days
(Revised 2001)
Date of
orbital determination
Determination
Orbital
Inclination
(deg)
Nodal
period
(min)
2001
2001
2000
2001
2001
2001
2001
2001
2001
2001
2001
2001
2001
2001
2001
2001
2001
2001
1999
2001
2001
2001
2001
2001
1999
2001
2001
2001
2001
Dec
Dec
Apr
Dec
Dec
Dec
Dec
Dec
Dec
Dec
Dec
Dec
Dec
Dec
Jun
Dec
Dec
Dec
Mar
Dec
Dec
Dec
Dec
Dec
Nov
Dec
Dec
Dec
Dec
17.36
17.45
22.25
16.65
16.62
16.71
16.97
16.83
16.87
16.94
16.82
17.44
16.81
16.95
21.48
16.95
16.76
17.20
31.11
17.22
16.99
16.39
17.55
17.23
16.40
16.58
16.64
17.14
17.39
71.09
70.66
70.97
71.11
71.13
71.12
70.95
71.18
71.13
71.17
70.99
71.03
71.18
71.27
71.05
71.17
71.30
70.60
71.24
71.12
71.23
70.91
70.84
71.18
71.25
71.35
71.52
71.34
71.35
103.32
102.20
92.97
97.38
98.28
102.92
102.57
103.13
103.27
103.42
99.25
102.43
103.18
103.27
88.30
103.52
102.35
97.33
89.17
98.65
103.40
102.22
103.20
102.13
90.45
102.23
100.08
100.87
101.73
2001
2001
2001
2001
2001
Dec
Dec
Dec
Dec
Dec
16.84
16.95
16.41
16.33
17.53
71.20
71.10
71.12
71.32
71.27
2001
2001
2001
2001
2001
2001
2000
2001
2001
1993
Dec
Jan
Dec
Dec
Dec
Dec
Mar
Dec
Dec
Jun
16.41
21.58
17.49
16.56
17.52
17.27
30.36
16.35
16.64
23.01
2001 Dec 17.04
2001 Dec 16.64
Semi
major axis
(km)
Extra Page 1992 - 5
Perigee
height
(km)
Apogee
height
(km)
Orbital
Argument
eccentricity of perigee
(deg)
7294
7242
6798
7012
7055
7275
7259
7285
7291
7299
7102
7252
7288
7292
6569
7304
7248
7010
6612
7072
7298
7242
7289
7239
6675
7250
7141
7178
7219
835
790
394
574
594
803
822
841
810
839
649
802
837
840
179
839
755
603
229
614
831
774
830
778
280
786
705
764
768
995
936
445
694
759
989
939
972
1015
1002
797
945
982
987
202
1011
984
659
237
773
1007
952
990
942
313
957
820
835
914
0.011
0.010
0.004
0.009
0.012
0.013
0.008
0.009
0.014
0.011
0.010
0.010
0.010
0.010
0.002
0.012
0.016
0.004
0.0006
0.011
0.012
0.012
0.011
0.011
0.003
0.012
0.008
0.005
0.010
334
121
201
245
249
135
349
246
189
279
31
220
254
184
224
293
341
336
213
285
218
346
58
86
328
115
259
107
57
102.95
102.92
102.32
102.67
102.38
7277
7275
7257
7264
7249
833
773
803
826
822
964
1020
954
944
919
0.009
0.017
0.010
0.008
0.007
204
188
279
83
72
71.13
70.91
70.80
70.92
70.89
71.28
70.57
70.85
71.20
70.51
103.43
88.83
104.33
103.17
103.38
103.47
91.92
102.88
102.67
90.43
7299
6596
7341
7287
7297
7301
6747
7274
7264
6674
822
206
830
827
805
793
345
841
786
267
1019
228
1095
989
1031
1052
392
949
984
324
0.013
0.002
0.018
0.011
0.015
0.018
0.003
0.007
0.014
0.004
185
35
130
307
42
283
146
350
247
230
70.77
70.39
101.53
101.47
7209
7207
772
754
890
902
0.008
0.010
18
267
RAE Table of Earth Satellites
Year of Launch 1992
Cospar ID
D
D
D
D
[Norad number]
1992-93 FD
[22464]
1992-93 FE
[22465]
1992-93 FF
[22466]
1992-93 FG
[22467]
1992-93 FH
[22468]
1992-93 FJ
[22469]
D 1992-93 FK
[22470]
1992-93 FL
[22471]
D 1992-93 FM
[22472]
1992-93 FN
[22473]
1992-93 FP
[22474]
1992-93 FQ
[22475]
1992-93 FR
[22476]
1992-93 FS
[22477]
1992-93 FT
[22478]
D 1992-93 FU
[22479]
1992-93 FV
[22480]
1992-93 FW
[22481]
D 1992-93 FX
[22482]
D 1992-93 FY
[22483]
D 1992-93 FZ
[22484]
1992-93 GA
[22485]
D 1992-93 GB
[22492]
1992-93 GC
[22493]
1992-93 GD
[22494]
1992-93 GE
[22495]
1992-93 GF
[22496]
D 1992-93 GG
[22497]
1992-93 GH
[22498]
1992-93 GJ
[22499]
1992-93 GK
[22500]
1992-93 GL
[22501]
1992-93 GM
[22502]
1992-93 GN
[22503]
1992-93 GP
[22504]
1992-93 GQ
[22505]
1992-93 GR
[22506]
D 1992-93 GS
[22507]
D 1992-93 GT
[22508]
1992-93 GU
[22509]
D 1992-93 GV
[22510]
D 1992-93 GW
[22511]
1992-93 GX
[22537]
D 1992-93 GY
[22538]
D 1992-93 GZ
[22539]
D 1992-93 HA
[22540]
D 1992-93 HB
[22541]
D 1992-93 HC
[22542]
1992-93 HD
[22543]
1992-93 HE
[22544]
2004 December 31 – version 1.01
Descent date
2001
2001
2001
2001
Apr
Jan
Mar
Aug
Lifetime
1
8
16
24
3019
2936
3003
3164
days
days
days
days
2000 May 20
2703 days
2003 Oct 24
3955 days
1996 May 4
1226 days
2000 Apr 20
1993 Feb 22
2001 Nov 13
2673 days
59 days
3245 days
1999 Jan 2
2199 days
1999 May 22
2730 days
2329 days
1998 Mar 3
2003 Oct 14
1894 days
3945 days
2003
1998
2000
1998
2000
3961
2100
2789
2085
2759
30
25
14
10
15
Orbital
Inclination
(deg)
2001
2001
2001
2001
2001
2001
2000
2001
2001
2001
2001
2001
2001
2001
2001
31.96
5.57
16.54
8.44
17.16
17.42
19.98
16.27
16.60
17.18
17.04
17.29
16.71
16.89
17.34
70.92
71.23
70.66
70.82
71.19
71.17
71.33
71.16
71.20
71.34
71.32
71.33
71.56
70.88
71.35
89.87
90.38
90.47
90.10
103.22
100.48
90.68
102.05
97.20
102.97
104.62
100.92
109.93
99.68
101.02
2001 Dec 16.29
2001 Dec 17.06
2000 Apr 17.91
71.14
71.29
71.42
2001 Nov 13.05
2001 Dec 17.00
2001
2001
2001
2001
Dec
Dec
Dec
Dec
2001
2001
2001
2001
2001
2001
2001
2001
2001
2000
1999
2001
Dec
Dec
Dec
Dec
Dec
Dec
Dec
Dec
Dec
Jun
May
Dec
Semi
major axis
(km)
Extra Page 1992 - 6
Perigee
height
(km)
Apogee
height
(km)
Orbital
Argument
eccentricity of perigee
(deg)
6647
6672
6676
6658
7289
7160
6687
7234
7003
7277
7355
7180
7602
7122
7185
262
292
281
275
804
747
291
776
557
789
821
753
833
666
747
274
295
314
284
1018
816
326
936
692
1008
1131
850
1613
821
866
0.0009
0.0002
0.002
0.0006
0.015
0.005
0.003
0.011
0.010
0.015
0.021
0.007
0.051
0.011
0.008
261
256
327
258
341
163
307
120
162
217
29
222
40
140
231
102.20
102.53
92.32
7241
7257
6767
785
785
370
941
971
406
0.011
0.013
0.003
134
255
227
71.09
70.47
89.77
102.48
6641
7255
256
770
268
982
0.0009
0.015
252
281
16.54
17.13
16.57
16.87
71.04
70.84
71.21
71.21
100.37
104.68
102.67
103.17
7155
7358
7264
7287
688
811
862
840
863
1147
908
976
0.012
0.023
0.003
0.009
77
276
249
235
16.06
16.74
17.51
17.44
16.82
17.11
17.50
18.10
17.90
14.99
12.22
17.34
71.28
71.43
70.85
70.97
70.81
71.21
71.33
70.82
70.68
70.99
70.92
71.14
101.12
102.55
101.55
101.25
103.92
101.43
102.23
101.40
101.97
92.20
90.02
102.87
7190
7257
7210
7196
7322
7205
7243
7203
7230
6761
6653
7272
749
792
782
790
829
785
784
752
792
363
272
798
874
965
882
876
1057
868
944
897
911
402
278
989
0.009
0.012
0.007
0.008
0.016
0.006
0.011
0.010
0.008
0.003
0.0004
0.013
306
115
353
193
62
140
120
342
70
247
352
158
2001 Dec 17.88
2001 Dec 17.58
2001 Dec 18.20
70.53
71.18
71.04
100.38
103.35
100.57
7155
7296
7164
731
822
727
821
1012
843
0.006
0.013
0.008
114
319
181
2000 Aug 13.27
70.95
91.45
6724
336
355
0.001
181
2000 Jul 14.50
2001 Dec 17.09
2001 Dec 17.92
70.67
71.35
71.27
91.00
102.82
103.43
6703
7271
7300
307
798
775
341
986
1067
0.003
0.013
0.020
264
176
294
Mar
Jan
Mar
Aug
Dec
Dec
May
Dec
Dec
Dec
Dec
Dec
Dec
Dec
Dec
Nodal
period
(min)
2339 days
2000 Jun 16
1999 May 12
Oct
Sep
Aug
Sep
Jul
(Revised 2001)
Date of
orbital determination
Determination
days
days
days
days
days
RAE Table of Earth Satellites
Year of Launch 1992
Cospar ID
D
D
D
D
1992-93
1992-93
1992-93
1992-93
1992-93
1992-93
1992-93
1992-93
1992-93
1992-93
1992-93
1992-93
1992-93
1992-93
1992-93
1992-93
1992-93
1992-93
1992-93
1992-93
1992-93
1992-93
1992-93
1992-93
1992-93
1992-93
1992-93
1992-93
1992-93
1992-93
1992-93
1992-93
1992-93
[Norad number]
HF
HG
HH
HJ
HK
HL
HM
HN
HP
HQ
HR
HS
HT
HU
HV
HW
HX
HY
HZ
JA
JB
JC
JD
JE
JF
JG
JH
JJ
JK
JL
JM
JN
JP
[22545]
[22546]
[22547]
[22548]
[22549]
[22550]
[22551]
[22552]
[22553]
[22554]
[22555]
[22556]
[22571]
[22572]
[22573]
[22574]
[22598]
[22660]
[22662]
[22665]
[22812]
[22816]
[22846]
[23008]
[23275]
[23282]
[23302]
[26979]
[26980]
[27749]
[27750]
[27751]
[28042]
Descent date
1993 May 19
Orbital
Inclination
(deg)
Nodal
period
(min)
2001 Dec 18.83
2001 Dec 17.09
2001 Dec 17.09
71.57
71.36
71.46
108.67
102.73
102.22
2001
2001
2001
2001
2001
2001
2001
2001
2001
2001
2001
2001
2001
2001
2001
2001
2001
2001
2001
1999
2001
2001
2001
2002
2002
2004
2004
2004
2004
71.22
71.22
70.87
71.09
71.44
71.39
70.52
70.63
71.36
70.72
71.01
71.08
70.65
70.95
70.52
71.08
70.69
71.49
70.65
70.98
71.25
71.17
71.13
71.32
71.12
71.11
71.16
71.17
70.88
103.12
101.18
103.25
101.48
100.60
102.42
102.00
97.20
103.80
100.77
101.27
103.47
103.12
95.30
102.25
102.73
103.78
103.67
94.33
91.52
103.37
102.85
103.10
101.68
102.52
102.47
102.12
101.05
102.47
Semi
major axis
(km)
Extra Page 1992 - 7
Perigee
height
(km)
Apogee
height
(km)
Orbital
Argument
eccentricity of perigee
(deg)
7543
7266
7242
823
790
782
1507
985
944
0.045
0.013
0.011
289
156
57
7284
7193
7291
7207
7166
7251
7232
7004
7317
7173
7197
7301
7264
6911
7244
7266
7316
7311
6865
6727
7297
7272
7284
7217
7257
7254
7238
7187
7254
810
718
842
790
760
793
769
592
791
747
752
801
838
513
772
828
824
810
480
338
836
806
808
757
774
784
765
763
820
1001
911
982
868
814
953
938
658
1085
842
884
1043
974
552
958
947
1051
1054
493
360
1000
981
1002
919
982
967
954
854
930
0.013
0.013
0.010
0.005
0.004
0.011
0.012
0.005
0.020
0.007
0.009
0.017
0.009
0.003
0.013
0.008
0.016
0.017
0.0009
0.002
0.011
0.012
0.013
0.011
0.014
0.013
0.013
0.006
0.008
274
154
10
207
130
100
216
333
281
21
207
258
117
98
231
280
167
219
4
13
235
270
181
140
133
310
219
252
211
145 days
2004 Apr 21
4135 days
2001 Oct 29
1999 Dec 17
3230 days
2548 days
Cosmos 2229 fragments, 4 pieces, all have decayed
D 1992-95 D
[22303]
1993 Jan 18
D 1992-95 E
[22304]
1993 Jan 29
D 1992-95 F
[22305]
1993 Jan 18
D 1992-95 G
[22306]
1993 Jan 12
2004 December 31 – version 1.01
Lifetime
(Revised 2001)
Date of
orbital determination
Determination
20
31
20
14
days
days
days
days
Dec
Dec
Dec
Dec
Dec
Dec
Dec
Dec
Dec
Dec
Dec
Dec
Dec
Dec
Dec
Dec
Dec
Dec
Oct
Dec
Dec
Dec
Dec
Jan
Feb
Dec
Dec
Dec
Dec
18.51
18.18
17.53
17.33
17.35
17.69
18.18
18.21
17.07
18.15
17.55
17.52
17.28
18.29
18.00
17.50
18.31
17.55
21.49
16.49
17.47
17.91
17.37
31.75
02.53
24.12
30.53
28.99
30.84