RAE Table of Earth Satellites (extended)
(Compiled 2006)
Page 1995-1
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)
1995 Jan 10.26
> million years
Box+ 2 panels
3661
2.45x2.20
x4.20
21.8 span
1995
1995
1995
1995
1995
1995
1995
2010
10.90
12.06
13.00
13.37
14.46
16.52
19.82
23.06
26.39
15.72
4.70
0.21
0.17
0.01
0.04
1.49
1995 Jan 11.04
1996 Jun 27.37
26.50
26.24
Year of Launch 1995
Name
[Launcher]
Fragments
Cospar ID
[Norad #] Launchsite
Cospar ID
Intelsat 704
[Atlas-2AS]
1995-01 A
[23461]
CC
Jan
Jan
Jan
Jan
Jan
Jan
Mar
Dec
Nodal
period
(min)
737.15
817.40
1096.14
1573.23
1466.57
1436.87
1436.07
1451.85
27031
28959
35218
44808
42759
42180
42164
42473
Perigee
height
(km)
Apogee
height
(km)
Orbital
Argument
eccentricity of perigee
(deg)
306
4033
16563
35772
35787
35793
35772
36084
40999
41128
41116
41087
36974
35809
35799
36104
0.753
0.640
0.349
0.059
0.014
0.0002
0.0003
0.0002
180
179
179
185
178
178
3
91
165
111
40805
592
0.756
0.036
180
356
110
250
D
Atlas-2AS 2nd stage 1995-01 B
(Centaur 113)
[23462]
1995 Jan 10.26
534 days
1996 Jun 27
Cylinder
1835
10.1 long
3.05 dia
D
r
Express 1 *
[M3-S2]
1995-UNC1
[NNA]
KAG-M1
1995 Jan 15.57
0.12 day
1995 Jan 15.69
Cyl service
module 360
+ re-entry
Module 405
0.87
1.36
1.35
1.36
D
M-3S-2 kick stage
1995-UNC2
[NNA]
1995 Jan 15.57
0.13 day?
1995 Jan 15.7
Cone-cyl
40
1.2 long?
0.7 dia
Tsikada 1
[Kosmos-3M]
1995-02 A
[23463]
PLE
1995 Jan 24.16
Cylinder
825
2.1 long
2 dia
1995 Jan 24.22
1995 Jan 24.59
2010 Dec 22.82
82.93
82.93
82.93
104.90 7368
104.97 7371
104.92 7369
960
964
962
1019
1021
1020
0.004
0.004
0.004
287
291
6
Astrid
1995-02 B
[23464]
1995 Jan 24.16
Box+ 4 panels
28
0.39x0.39
x0.29
1.08 span
1995 Jan 24.81
2010 Dec 23.95
82.93
82.93
105.00 7373
104.93 7370
964
960
1025
1022
0.004
0.004
290
13
FAISAT
1995-02 C
[23465]
1995 Jan 24.16
Octagonal cyl
114
0.89 long
0.46 dia
1995 Jan 24.81
2010 Dec 23.95
82.94
82.93
104.98 7373
104.97 7371
967
964
1020
1021
0.004
0.004
289
15
Kosmos-3M 2nd stage 1995-02 D
[23466]
1995 Jan 24.16
Cylinder
1434
4.21 long
2.4 to
3.2 maxdia
1995 Jan 24.88
2010 Dec 24.05
82.92
82.92
104.85 7368
104.78 7363
964
959
1010
1009
0.003
0.003
289
315
*
long
maxdia
long
maxdia
730.32 26064
91.57 6730
33
Not catalogued by USSPACECOM. The re-entry module landed in Ghana in stead of at Woomera, Australia; and was discovered after about 5.5 days.
2nd stage lost altitude control. Capsule re-entered on its 3rd orbit.
RAE Table of Earth Satellites (extended)
(Compiled 2006)
Page 1995-2
Launchdate
Lifetime + Descent date
[Norad]
Shape and
weight (kg)
Descent date
Size
(m)
Lifetime
Date of
orbital
determination
Orbital
Inclination
(deg)
Semi
major axis
(km)
Year of Launch 1995
Name
[Launcher]
Fragments
Cospar ID
[Norad #] Launchsite
Cospar ID
Jan
Jan
Feb
Feb
Feb
Feb
Dec
Nodal
period
(min)
Orbital
Argument
eccentricity of perigee
(deg)
290
313
7495
24473
34225
35646
35769
27521
36042
35968
36387
35947
35929
35803
0.671
0.727
0.506
0.161
0.021
0.003
0.0004
174
177
176
175
174
183
233
289
262
27445
23023
0.671
0.632
183
100
1995-03 A
[23467]
CC
1995 Jan 29.06
> million years
Box+ 2 panels
2800 full
1360 os
2.7x2.2
x2.6
6.8 high
26.5 span
1995
1995
1995
1995
1995
1995
1997
29.36
31.69
1.69
2.81
4.02
10.50
31.46
26.62
26.69
14.67
5.39
5.24
5.14
4.05
Atlas-2 2nd stage
(Centaur 112)
1995-03 B
[23468]
1995 Jan 29.06
Cylinder
1815
10.1 long
3.05 dia
1995 Feb 7.85
2010 Dec 22.63
26.94
26.57
D STS-063
6M Discovery F20
R [Shuttle]
1995-04 A
[23469]
CC-LC39B
1995 Feb 3.22
8.27 days
1995 Feb 11.49
Delta wing
78796 empty
95852 landing
37.3 long
5.5 dia
23.8 span
1995
1995
1995
1995
1995
1995
51.66
51.65
51.65
51.65
51.65
51.65
90.98
91.40
91.62
92.05
92.33
92.30
6701
6722
6732
6754
6768
6766
305
332
332
368
387
385
340
354
375
382
391
390
0.003
0.002
0.003
0.001
0.0003
0.0003
203
293
292
19
217
165
D
R
Spartan 204 *
1995-04 B
[23470]
1995 Feb 3.22
8.27 days
1995 Feb 11.49
1167
1995 Feb 8.13
1995 Feb 8.51
51.65
51.65
92.32 6767
92.32 6766
388
387
388
388
0.00002
0.00005
287
249
D
ODERACS 2A #
1995-04 C
[23471]
1995 Feb 3.22
404 days
1996 Mar 13
Sphere, black
aluminium
0.15 dia
1995 Feb 8.42
51.65
91.33 6718
328
351
0.002
323
D
ODERACS 2B #
1995-04 D
[23472]
1995 Feb 3.22
239 days
1995 Sep 29
Sphere, white
aluminium
0.10 dia
1995 Feb 5.18
1995 Sep 28.47
51.65
51.63
91.27 6715
88.05 6556
324
177
349
179
0.002
0.0002
326
274
D
ODERACS 2C #
1995-04 E
[23473]
1995 Feb 3.22
369 days
1996 Feb 7
Sphere, stain- 0.05 dia
less steel
No TLE issued.
D
ODERACS 2D #
1995-04 F
[23474]
1995 Feb 3.22
27 days
1995 Mar 2
dipole
0.134x0.01
platinum alloy
1995 Feb 9.81
1995 Feb 24.25
51.65
51.64
91.10 6707
89.62 6634
318
246
338
254
0.001
0.001
344
167
D
ODERACS 2E #
1995-04 G
[23475]
1995 Feb 3.22
24 days
1995 Feb 27
dipole
0.134x0.01
platinum alloy
1995 Feb 11.14
1995 Feb 24.86
51.64
51.63
91.12 6708
89.82 6644
319
261
339
269
0.001
0.0006
337
155
D
ODERACS 2F #
1995-04 H
[NNA]
1995 Feb 3.22
17 days
1995 Feb 20
dipole
0.044x0.01
platinum alloy
*
#
Deployed attached to shuttle arm 1995 Feb 4; released 1995 Feb 7.52 and re-captured 1995 Feb 9.48.
Second flight of Orbital DEbris RAdar Calibration System.
3.28
4.21
4.60
5.78
6.85
10.92
20284
24556
28110
36809
41464
42165
42165
Apogee
height
(km)
UFO 4
(USA 108)
[Atlas-2 8112]
Feb
Feb
Feb
Feb
Feb
Feb
479.17
638.25
781.73
1171.35
1400.47
1436.10
1436.10
Perigee
height
(km)
477.80 20245
401.27 18021
RAE Table of Earth Satellites (extended)
(Compiled 2006)
Page 1995-3
Launchdate
Lifetime + Descent date
[Norad]
Shape and
weight (kg)
Descent date
Semi
major axis
(km)
Year of Launch 1995
Name
[Launcher]
Fragments
Cospar ID
[Norad #] Launchsite
Cospar ID
Size
(m)
Lifetime
Date of
orbital
determination
Orbital
Inclination
(deg)
Nodal
period
(min)
Perigee
height
(km)
Apogee
height
(km)
Orbital
Argument
eccentricity of perigee
(deg)
D
Progress-M 26 $
[Soyuz-U]
1995-05 A
[23477]
BAI
1995 Feb 15.70
28 days
1995 Mar 15
Cyl+ 2 panels+ 7.9 long
1995 Feb 15.75
beehive+sphere 2.72 maxdia 1995 Feb 16.00
7250
1995 Feb 17.62
1995 Mar 15.02
51.61
51.65
51.65
51.64
88.60
89.83
89.90
92.42
6584
6645
6648
6772
187
238
246
390
223
294
294
396
0.003
0.004
0.004
0.0004
93
125
131
255
D
Soyuz-U 3rd stage
(Block I)
1995-05 B
[23478]
1995 Feb 15.70
2 days
1995 Feb 17
Cylinder
2400
8.1 long
2.66 dia
1995 Feb 15.69
1995 Feb 17.65
51.63
51.60
88.52 6579
87.12 6510
187
126
214
137
0.002
0.0008
91
159
D
R
Foton 7 (F10)
[Soyuz-U]
1995-06 A
[23497]
PLE
1995 Feb 16.74
15.62 days
1995 Mar 3.36
Stubby cil+
sphere+double
cone
6200
5.5 long
2.4 maxdia
1995 Feb 17.04
1995 Mar 3.15
62.81
62.80
90.38 6672
90.27 6666
219
218
368
357
0.011
0.010
107
108
D
Soyuz-U 3rd stage
(Block I)
1995-06 B
[23498]
1995 Feb 16.74
24 days
1995 Mar 12
Cylinder
2800
8.1 long
2.66 dia
1995 Feb 16.93
1995 Mar 12.73
62.80
62.78
90.33 6670
87.25 6517
219
133
363
144
0.011
0.0008
107
120
D
Retrorocket
Casing
1995-06 D
[23503]
1995 Feb 16.74
26 days
1995 Mar 14
1995 Mar 3.92
1995 Mar 14.47
62.83
62.80
92.40 6771
88.78 6593
309
196
475
233
0.012
0.003
15
359
D
Retrorocket
Casing
1995-06 E
[23504]
1995 Feb 16.74
44 days
1995 Apr 1
1995 Mar 4.17
1995 Mar 18.89
1995 Apr 1.19
62.80
62.79
62.80
92.15 6758
91.32 6718
87.55 6532
308
288
150
452
391
157
0.011
0.008
0.0005
25
24
354
D
Battery module
1995-06 G
[23506]
1995 Feb 16.74
58 days
1995 Apr 15
Cylinder
500
1 long
1.7 dia
1995 Mar 4.28
1995 Mar 24.21
1995 Apr 14.78
62.80
62.80
62.79
90.22 6664
89.63 6635
87.47 6527
217
208
141
354
305
156
0.010
0.007
0.001
108
107
106
D
D
Fragment
1995-06 C
1995-06 F
[23499]
[23505]
1995 Feb 18
2 days
1995 Mar 14
26 days
1995 Feb 18.23
1995 Mar 3.78
1995 Mar 13.65
62.79
62.80
62.75
89.77 6641
90.07 6556
88.20 6564
205
215
160
320
340
210
0.009
0.009
0.004
110
113
117
Delta wing
98740
37.3 long
5.5 dia
23.8 span
1995 Mar 2.31
1995 Mar 10.25
1995 Mar 17.58
28.47
28.47
28.47
91.58 6731
91.55 6729
91.53 6728
346
341
336
358
360
363
0.0009
0.001
0.002
257
16
114
D STS-067 *
7M Endeavour F8
R [Shuttle]
$
*
1995-07 A
[23500]
CC-LC39
1995 Mar 2.28
16.63 days
1995 Mar 18.91
Docked with MIR (Kvant-1 port) 1995 Feb 17.77 and undocked 1995 Mar 15.10
ASTRO 2 mission with 7 astronauts (Oswald, Gregory, Grunsfeld, Lawrence, Jernigan, Durrance and Parise). Landed at Edwards AFB
RAE Table of Earth Satellites (extended)
(Compiled 2006)
Page 1995-4
Launchdate
Lifetime + Descent date
[Norad]
Shape and
weight (kg)
Descent date
Semi
major axis
(km)
1995-08 A
[23501]
PLE
1995 Mar 2.54
2069 days
2000 Oct 30
1000
D
Kosmos-3M 2nd stage 1995-08 B
[23502]
1995 Mar 2.54
1935 days
2000 Jun 18
D
Sub-satellite 1
1995-08 C
[23507]
D
Sub-satellite 2
D
Year of Launch 1995
Name
[Launcher]
Fragments
Date of
orbital
determination
Orbital
Inclination
(deg)
Perigee
height
(km)
Apogee
height
(km)
Orbital
Argument
eccentricity of perigee
(deg)
1995 Mar 2.86
2000 Oct 30.40
65.85
65.81
94.47 6871
87.30 6519
469
137
516
145
0.003
0.0006
345
269
1995 Mar 2.86
2000 Jun 18.48
65.85
65.80
94.35 6866
87.47 6527
460
138
515
159
0.004
0.002
350
268
1995 Mar 2.54
954 days
1997 Oct 11
1995 Mar 6.09
1997 Oct 11.08
65.85
65.83
94.82 6888
89.13 6611
477
224
543
240
0.005
0.001
313
226
1995-08 D
[23508]
1995 Mar 2.54
486 days
1996 Jun 30
1995 Mar 6.39
1996 Jun 30.41
65.81
65.79
94.17 6857
88.22 6564
441
179
515
192
0.005
0.001
350
234
Sub-satellite 3
1995-08 E
[23509]
1995 Mar 2.54
419 days
1996 Apr 24
1995 Mar 7.11
1996 Apr 24.21
65.83
65.80
94.08 6852
88.65 6586
434
198
514
218
0.006
0.002
340
194
D
Sub-satellite 4
1995-08 F
[23510]
1995 Mar 2.54
412 days
1996 Apr 17
1995 Mar 7.11
1996 Apr 16.32
65.89
65.85
94.07 6582
88.87 6597
433
212
514
224
0.006
0.0009
343
314
D
Sub-satellite 5
1995-08 G
[24781]
1995 Mar 2.54
1366 days
1998 Nov 27
1997 Apr 22.03
1998 Nov 27.12
65.86
65.83
94.45 6870
88.90 6599
469
216
515
224
0.003
0.0006
244
58
D
Sub-satellite 6
1995-08 H
[24782]
1995 Mar 2.54
1352 days
1998 Nov 13
1997 Apr 22.03
1998 Nov 12.59
65.84
65.81
94.38 6868
88.08 6558
463
175
515
185
0.004
0.0008
242
251
D
Sub-satellite 7
1995-08 J
[24783]
1995 Mar 2.54
1328 days
1998 Oct 20
1997 Apr 22.03
1998 Oct 19.93
65.86
65.82
94.28 6862
88.42 6575
453
187
515
206
0.005
0.001
240
280
D
Sub-satellite 8
1995-08 K
[24784]
1995 Mar 2.54
1311 days
1998 Oct 3
1997 Apr 22.03
1998 Oct 3.73
65.83
65.80
94.23 6860
87.40 6525
448
122
514
170
0.005
0.004
239
209
D
Sub-satellite 9
1995-08 L
[24785]
1995 Mar 2.54
1341 days
1998 Nov 2
1997 Apr 22.28
1998 Nov 2.08
65.87
65.84
94.33 6865
88.28 6568
458
181
514
197
0.004
0.001
241
316
D
Sub-satellite 10
1995-08 M
[24789]
1995 Mar 2.54
1342 days
1998 Nov 3
1997 Apr 26.01
1998 Nov 2.65
65.83
65.80
94.33 6865
88.48 6578
458
191
514
208
0.004
0.001
239
39
D
Fragments
1995-08 N-AA 13 pieces, all have decayed
D
Cospar ID
[Norad #] Launchsite
Cospar ID
Cosmos 2306
[Kosmos-3M]
Cylinder
1434
Size
(m)
Lifetime
4.21 long
2.4 dia
Nodal
period
(min)
For orbital information see extra pages at end of year
RAE Table of Earth Satellites (extended)
(Compiled 2006)
Page 1995-5
Launchdate
Lifetime + Descent date
[Norad]
Shape and
weight (kg)
Descent date
Semi
major axis
(km)
Year of Launch 1995
Name
[Launcher]
Fragments
Cospar ID
[Norad #] Launchsite
Cospar ID
Size
(m)
Lifetime
Date of
orbital
determination
Orbital
Inclination
(deg)
Nodal
period
(min)
Perigee
height
(km)
Apogee
height
(km)
Orbital
Argument
eccentricity of perigee
(deg)
Cosmos 2307
(Glonass 73)
[Proton-K]
1995-09 A
[23511]
BAI
1995 Mar 7.39
1 million years
Cyl +2 panels
1300
1995 Mar 7.40
1995 Mar 9.75
1995 Mar 18.66
64.76
64.80
64.79
676.97 25539
676.08 25517
675.72 25508
19126
19128
19116
19196
19148
19142
0.001
0.004
0.0005
177
183
224
Cosmos 2308
(Glonass 71)
1995-09 B
[23512]
1995 Mar 7.39
1 million years
Cyl +2 panels
1300
1995
1995
1995
1995
1995
1995
Mar
Mar
Mar
Mar
Mar
Mar
3.40
9.80
15.13
16.82
24.88
26.76
64.87
64.81
64.78
64.78
64.78
64.78
676.27
676.08
682.32
684.10
678.22
675.73
25521
25517
25674
25719
25571
25508
19128
19131
19140
19140
19134
19113
19157
19146
19450
19540
19250
19147
0.0006
0.0003
0.006
0.008
0.002
0.007
176
174
89
88
69
332
Cosmos 2309
(Glonass 72)
1995-09 C
[23513]
1995 Mar 7.39
1 million years
Cyl +2 panels
1300
1995
1995
1995
1995
1995
Mar
Mar
Mar
Mar
Mar
7.40
9.75
16.77
17.25
21.89
64.87
64.80
64.79
64.79
64.79
675.82
676.12
667.50
674.05
675.73
25510
25518
25301
25466
25508
19117
19127
18702
19033
19100
19146
19152
19142
19141
19159
0.0006
0.0005
0.009
0.002
0.001
176
191
262
250
203
D
Proton-K 3rd stage
1995-09 D
[23514]
1995 Mar 7.39
4 days
1995 Mar 11
Cylinder
4185
4 long
4.1 dia
1995 Mar 7.45
64.80
87.65 6537
141
175
0.003
304
D
Proton-K 4th stage
Casing
1995-09 E
[23515]
1995 Mar 7.39
< 0.6 day
1995 Mar 7
Hollow cyl
800
4.0 long
3.7 dia
1995 Mar 7.87
64.80
87.15 6512
125
142
0.001
270
Proton-K 4th stage
(Block DM-2)
1995-09 F
[23516]
1995 Mar 7.39
1 million years
Cylinder
2350
6.22 long
3.7 maxdia
1995 Mar 8.81
64.76
675.05 25491
19089
19137
0.0009
268
Ullage motor
1995-09 G
[23517]
1995 Mar 7.39
Cylinder
55
0.90 long
0.68 dia
1995 Mar 9.10
64.78
340.25 16145
388
19145
0.581
297
Ullage motor
1995-09 H
[23518]
1995 Mar 7.39
Cylinder
55
0.90 long
0.68 dia
1995 Mar 9.10
64.85
340.22 16144
385
19145
0.581
297
RAE Table of Earth Satellites (extended)
(Compiled 2006)
Page 1995-6
Launchdate
Lifetime + Descent date
[Norad]
Shape and
weight (kg)
Descent date
Semi
major axis
(km)
1995-10 A
[23519]
BAI
1995 Mar 14.26
181.03 days
1995 Sep 11.29
Cyl+ 2 panels+ 7.9 long
1995 Mar 14.26
beehive+sphere 2.72 maxdia 1995 Mar 15.18
7150
1995 Mar 16.88
1995 Sep 10.04
51.82
51.65
51.65
51.64
88.73
89.85
92.42
92.35
Year of Launch 1995
Name
[Launcher]
Fragments
Cospar ID
[Norad #] Launchsite
Cospar ID
D Soyuz-TM 21 *
3M [Soyuz-U2]
R
Size
(m)
Lifetime
Date of
orbital
determination
Orbital
Inclination
(deg)
Nodal
period
(min)
Perigee
height
(km)
Apogee
height
(km)
Orbital
Argument
eccentricity of perigee
(deg)
6590
6645
6772
6773
194
228
390
392
229
306
396
398
0.003
0.006
0.0004
0.0004
95
129
263
54
D
Soyuz-U2 3rd stage
(Block I)
1995-10 B
[23520]
1995 Mar 14.26
2 days
1995 Mar 16
Cylinder
2400
8.1 long
2.66 dia
1995 Mar 15.01
1995 Mar 16.70
51.63
51.62
88.48 6578
87.48 6528
189
148
211
151
0.002
0.0002
85
82
D
Space Flyer Unit # 1995-11 A
[H-2]
[23521]
TAN
1995 Mar 18.33
289.99 days
1996 Jan 20.32
8-sided
stubby cyl
4000
4.46 dia
2.8 high
24.4 span
1995
1995
1995
1995
1995
1995
1995
1996
1996
Mar
Apr
Jun
Jul
Oct
Dec
Dec
Jan
Jan
19.27
28.86
1.03
3.34
19.47
21.81
23.83
11.68
18.65
28.46
28.45
28.45
28.45
28.46
28.45
28.45
28.45
28.45
91.03
94.17
93.45
92.20
94.02
94.32
94.07
94.07
94.07
6704
6857
6822
6761
6849
6864
6852
6852
6852
312
464
441
373
461
480
469
469
469
339
492
446
392
480
490
478
478
478
0.002
0.002
0.0004
0.001
0.001
0.0007
0.0006
0.0006
0.0006
315
37
32
87
189
234
325
166
244
Himawari 5
(GMS 5)
1995-11 B
[23522]
1995 Mar 18.33
> million years
Cylindrical
746
2.15 dia
3.54 high
1995
1995
1995
1995
2010
Mar
Mar
Apr
Apr
Dec
19.04
19.65
1.21
15.20
22.76
25.15
1.06
1.06
1.03
8.81
647.32
1419.05
1434.73
1436.07
1448.65
24788
41830
42138
42164
42410
353
34583
35730
35783
36000
36466
36321
35789
35788
36063
0.728
0.021
0.0007
0.00006
0.0007
180
221
304
317
339
H-2 2nd stage
1995-11 C
[23523]
1995 Mar 18.33
Spheroid +
cyl + cone
2800
10.3 long
4 maxdia
1995 Apr 8.57
2010 Dec 22.80
25.57
25.19
582.95 23116
496.57 20772
292
281
33184
28506
0.711
0.679
190
21
Himawari 5 AKM
(Star-27)
1995-11 D
[23524]
1995 Mar 18.33
Sphere+cone
30
1.3 long
0.7 dia
1995 Mar 18.90
2010 Dec 15.07
1.09
11.28
1422.28 41894
1422.12 41891
34611
34534
34420
36490
0.022
0.023
221
216
Lower Payload
Shroud
1995-11 E
[23525]
1995 Mar 18.33
22 days
1995 Apr 9
Hollow cyl
500
4 long
4 dia
1995 Mar 19.14
1995 Apr 9.13
28.45
28.45
91.05 6704
88.88 6598
311
218
340
220
0.002
0.0002
303
107
D
1995 11 continued on next page.
*
#
Crew of Dezhurov, Strekalov and Thagard docked with MIR (Kvant 1 port) 1995 Mar 16.31; they returned to earth aboard the shuttle Atlantis (1995-030A);
Undocking 1995 Jul 4.47 and landing 1995 Jul 7.62 at KSC. Soyuz-TM 21, with cosmonauts Solovyov and Budarin who had flown to MIR with Atlantis, undocked
From MIR 1995 Jul 4.45 and observed the undocking of Atlantis from a distance of 100 m; re-docking 1995 Jul 4.49; finally undocked 1995 Sep 11.15.
Recovered by STS-072 shuttle mission, grappled by the robot arm 1996 Jan 13.46 and returned to Earth.
RAE Table of Earth Satellites (extended)
(Compiled 2006)
Page 1995-7
Launchdate
Lifetime + Descent date
[Norad]
Shape and
weight (kg)
Descent date
Size
(m)
Lifetime
Date of
orbital
determination
Orbital
Inclination
(deg)
Semi
major axis
(km)
Year of Launch 1995
Name
[Launcher]
Fragments
D
Cospar ID
[Norad #] Launchsite
Cospar ID
Nodal
period
(min)
Perigee
height
(km)
Apogee
height
(km)
Orbital
Argument
eccentricity of perigee
(deg)
SFU solarpanel #
1995-11 J
[23771]
1995 Mar 18.33
1310 days
1998 Oct 18
Plate
2.4x9.8
1996 Jan 17.02
1997 Mar 17.04
1998 Oct 17.67
28.45
28.45
28.39
94.05 6851
93.80 6839
88.50 6579
468
457
197
477
463
204
0.0006
0.0005
0.0005
229
291
240
SFU solarpanel #
1995-11 K
[23772]
1995 Mar 18.33
1351 days
1998 Nov 28
Plate
2.4x9.8
1996 Jan 17.87
1997 Mar 17.11
1998 Nov 28.40
25.45
28.45
28.47
94.05 6851
93.83 6840
87.77 6542
469
458
138
476
465
189
0.0005
0.0005
0.004
232
288
63
Fragments
1995-11 F
[23569]
1995 Jul 12
129 days
1997 May 21
795 days
1995 Nov 21
230 days
1995
1995
1995
1997
1995
1995
28.86
12.21
16.19
21.11
3.34
21.31
28.45
28.46
28.46
28.45
28.45
28.28
94.17
89.45
94.18
87.97
92.20
87.67
6857
6626
6857
6553
6761
6538
464
240
164
174
373
158
492
254
193
174
392
160
0.002
0.001
0.002
0
0.001
0.0002
37
130
254
214
87
210
Cosmos 2310
[Kosmos-3M]
1995-11 G
[23570]
1995-11 H
[23593]
Apr
Jul
Apr
May
Jul
Nov
1995-12 A
[23526]
PLE
1995 Mar 22.17
Cylinder
825
2.1 long
2 dia
1995 Mar 22.23
2010 Dec 24.02
82.94
82.94
105.02 7374
104.97 7372
980
976
1010
1010
0.002
0.002
265
142
Kosmos-3M 2nd stage 1995-12 B
[23527]
1995 Mar 22.17
Cylinder
1434
4.21 long
2.4 dia
1995 Mar 22.45
2010 Dec 24.08
82.93
82.94
104.88 7368
104.85 7366
978
971
1000
1003
0.001
0.002
239
64
Intelsat 705
[Atlas-2AS]
1995 Mar 22.26
> million years
Box+ 2 panels
3660
2.45x2.20
x4.20
21.8 span
1995
1995
1995
1995
1995
1995
2010
22.54
25.63
28.06
29.92
31.92
21.24
22.38
26.49
5.49
0.05
0.07
0.06
0.07
1.02
170
14820
35498
35502
35613
35618
35771
40208
40189
40162
36106
36105
35952
35802
0.754
0.374
0.053
0.007
0.006
0.004
0.0004
178
180
216
198
171
209
197
1995 Jan 10.26
1417 days
1999 Feb 6.53
Cylinder
1835
10.1 long
3.05 dia
1995 Mar 22.53
1999 Feb 6.35
26.53
26.50
169
106
39882
403
0.752
0.022
179
296
1995-13 A
[23528]
CC
Mar
Mar
Mar
Mar
Mar
Apr
Dec
718.27
1034.50
1541.77
1437.00
1439.83
1436.05
1436.12
26568
33883
44029
42183
42238
42164
42165
D
Atlas-2AS 2nd stage 1995-13 B
(Centaur 115)
[23529]
#
Solar panels did not latch against SFU body and were detached just before the capture. J released 1996 Jan 13.40 and K 1996 Jan 13.41
711.63 26404
89.60 6653
RAE Table of Earth Satellites (extended)
(Compiled 2006)
Page 1995-8
Launchdate
Lifetime + Descent date
[Norad]
Shape and
weight (kg)
Descent date
Size
(m)
Lifetime
Date of
orbital
determination
Orbital
Inclination
(deg)
Semi
major axis
(km)
Year of Launch 1995
Name
[Launcher]
Fragments
Cospar ID
[Norad #] Launchsite
Cospar ID
Perigee
height
(km)
Apogee
height
(km)
Orbital
Argument
eccentricity of perigee
(deg)
D
Cosmos 2311
[Soyuz-U]
1995-14 A
[23530]
PLE
1995 Mar 22.70
70.1 days
1995 May 31.8
Cylindrical?
6500
7 long
2.5 dia
1995
1995
1995
1995
1995
1995
1995
1995
1995
1995
1995
1995
1995
1995
1995
1995
1995
23.00
30.19
30.51
11.17
12.17
19.01
20.30
21.05
29.53
30.09
5.51
5.76
12.11
12.67
19.46
20.08
31.67
67.15
67.15
67.15
67.14
67.15
67.14
67.14
67.14
67.13
67.13
67.13
67.14
67.13
67.13
67.13
67.13
67.12
89.53
89.00
90.08
89.52
89.70
88.93
88.83
90.00
89.57
89.78
89.57
89.77
89.50
89.75
89.47
89.97
89.43
6630
6604
6657
6629
6638
6600
6595
6653
6631
6642
6631
6641
6628
6641
6626
6651
6625
169
161
172
166
178
173
172
176
171
182
179
179
176
185
182
186
177
334
289
385
336
340
269
261
373
335
346
327
347
322
339
314
359
315
0.012
0.010
0.016
0.013
0.012
0.007
0.007
0.015
0.012
0.012
0.011
0.013
0.011
0.012
0.010
0.013
0.010
92
85
63
53
60
58
57
111
101
108
102
102
95
141
133
122
109
D
Soyuz-U 3rd stage
(Block I)
1995-14 B
[23531]
1995 Mar 22.70
5 days
1995 Mar 27
Cylinder
2400
8.1 long
2.66 dia
1995 Mar 23.12
1995 Mar 27.19
67.14
67.14
89.37 6622
87.28 6518
169
123
318
156
0.011
0.003
90
81
D
Fragments
1995-14 C
[23591]
1995 Jun 1
71 days
1995 Jun 1
71 days
1995
1995
1995
1995
67.07
67.10
67.12
67.12
88.72
88.23
88.83
88.35
6589
6565
6595
6571
167
150
170
158
254
224
263
228
0.007
0.006
0.007
0.005
109
107
108
111
Box + panel
823
6.4 long
1.22 wide
1995 Mar 24.77
2009 Nov 30.46
101.92 7228
101.75 7220
846
836
853
847
0.0005
0.0008
264
119
D
1995-14 D
[23592]
Mar
Mar
Mar
Apr
Apr
Apr
Apr
Apr
Apr
Apr
May
May
May
May
May
May
May
Nodal
period
(min)
Jun
Jun
Jun
Jun
1.05
1.17
1.05
1.17
DMSP-2 8 (5D2 F13) 1995-15 A
(USA 109)
[23533]
[Atlas-E]
VDB
1995 Mar 24.59
Fragments
1995-15 B-E
4 pieces, all in orbit
Brasilsat B2
[Ariane-44LP]
1995-16 A
[23536]
KOU-ELA2
1995 Mar 28.97
> million years
Cylindrical
1780
3.6 dia
3.6 to
8.4 high
Mar
Mar
Apr
Apr
Apr
Dec
29.07
31.16
6.63
6.63
21.13
23.50
6.99
2.67
0.15
0.18
0.10
2.66
639.65
765.30
1424.68
1436.03
1436.08
1436.08
24592
27715
41941
42164
42164
42164
248
6766
35343
35769
35766
35776
36179
35907
35782
35801
35805
35795
0.731
0.526
0.005
0.0004
0.0005
0.0002
178
192
312
58
34
191
Hot Bird 1
1995-16 B
[23537]
1995 Mar 28.97
> million years
Box+ 2 panels
1800
2.8x2.2x2.5 1995 Mar
22.40 span 1995 Apr
1995 Apr
1995 Apr
2010 Dec
29.79
1.05
10.02
21.99
23.61
7.03
0.36
0.04
0.03
4.52
631.32
1330.30
1436.18
1436.05
1449.92
24378
40068
42167
42164
42435
227
31489
35780
35776
36049
35771
35889
35796
35795
36064
0.729
0.055
0.0002
0.0002
0.0002
179
177
302
309
166
1995 16 continued on next page
98.83
98.75
For orbital information see extra pages at end of year
1995
1995
1995
1995
1995
2010
RAE Table of Earth Satellites (extended)
(Compiled 2006)
Page 1995-9
Launchdate
Lifetime + Descent date
[Norad]
Shape and
weight (kg)
Descent date
Size
(m)
Lifetime
Date of
orbital
determination
Orbital
Inclination
(deg)
Semi
major axis
(km)
Year of Launch 1995
Name
[Launcher]
Fragments
D
Cospar ID
[Norad #] Launchsite
Cospar ID
Nodal
period
(min)
Perigee
height
(km)
Apogee
height
(km)
Orbital
Argument
eccentricity of perigee
(deg)
Ariane-4 41
3rd stage (H 10+)
+ VEB
+ Spe;da lower
Section
1995-16 C
[23538]
1995 Mar 28.97
Cylinder
1250
Cylinder
530
Hollow cyl
200
11.4 long
2.6 dia
1 long
dia
4 dia
1.5 high
1995 Mar 31.78
2010 Dec 21.92
6.74
6.40
653.43 24944
524.92 21556
297
295
36833
30059
0.732
0.690
181
298
Spelda
upper section
1995-16 D
[23539]
1995 Mar 28.97
1372 days
1998 Dec 29.13
Hollow cyl
210
1.3 long
4 dia
1995 Mar 29.21
1998 Dec 28.83
7.05
6.57
630.42 24355
94.08 6852
220
118
35732
830
0.729
0.052
178
339
ORBCOMM 1
[L-1011/Pegasus]
1995-17 A
[23545]
VDB
1995 Apr 3.58
Drum+2 panels 1.4 dia
+ gravity boom 0.165 deep
40
4.32 long
2.24 span
1995 Apr 3.76
2010 Dec 23.73
70.00
69.97
99.67 7121
98.50 7066
735
681
750
693
0.001
0.001
70
182
ORBCOMM 2
1995-17 B
[23546]
1995 Apr 3.58
Drum+2 panels 1.4 dia
+ gravity boom 0.165 deep
40
4.32 long
2.24 span
1995 Apr 4.04
2010 Dec 24.82
69.99
69.98
99.62 7119
98.52 7066
734
681
747
694
0.001
0.0009
80
163
Orbview 1
(ex Microlab 1)
1995-17 C
[23547]
1995 Apr 3.58
Drum
1.04 dia
0.38 high
+ gravity boom 5.5 long
+2 circ panels 0.96 dia
74
1995 Apr 4.11
2010 Dec 24.45
69.98
69.98
99.63 7119
98.92 7085
734
698
748
716
0.001
0.001
82
202
Pegasus 3rd stage
1995-17 D
[23548]
1995 Apr 3.58
Cylinder
200
2.08 long
0.965 dia
1995 Apr 4.24
2010 Dec 23.75
69.99
69.99
99.67 7121
99.37 7107
736
719
749
738
0.001
0.001
69
235
Fragment
1995-17 E
[23650]
2000 Aug 19
1965 days
1995 May 30.57
2000 Aug 18.30
70.00
69.94
99.60 7118
90.72 6689
729
291
750
329
0.001
0.003
1
194
D
Ofeq 3
[Shavit]
1995-18 A
[23549]
PAL
1995 Apr 5.47
2030 days
2000 Oct 25
Cone
225
0.7-2.3 dia 1995 Apr 5.79
2.3 high
2000 Oct 24.33
143.38
143.29
95.62 6927
88.47 6577
367
196
729
200
0.026
0.0003
74
203
D
Shavit 3rd stage
1995-18 B
[23550]
1995 Apr 5.47
142 days
1995 Aug 25
Cone-sphere
100
2.6 long
1.56 dia
143.38
143.35
94.37 6867
88.03 6555
246
156
731
197
0.035
0.003
76
277
1995 Apr 6.25
1995 Aug 25.40
RAE Table of Earth Satellites (extended)
(Compiled 2006)
Page 1995-10
Launchdate
Lifetime + Descent date
[Norad]
Shape and
weight (kg)
Descent date
Size
(m)
Lifetime
Date of
orbital
determination
Orbital
Inclination
(deg)
Semi
major axis
(km)
Year of Launch 1995
Name
[Launcher]
Fragments
Cospar ID
[Norad #] Launchsite
Cospar ID
Orbital
Argument
eccentricity of perigee
(deg)
219
10064
27483
35759
35779
35772
40161
40165
40164
35797
35793
35800
0.752
0.478
0.157
0.0004
0.0002
0.0003
178
178
178
213
336
199
207
115
40103
387
0.752
0.021
177
85
1995 Apr 7.99
> million years
Box+2 panels
+2 antennae
2700
3.63 across
4.4 high
20.96 span
18.9 across
1995
1995
1995
1995
1995
2010
8.27
11.85
13.90
19.63
23.43
22.21
26.43
9.03
2.87
0.09
0.04
5.84
D
Atlas-2A 2nd stage
(Centaur)
1995-19 B
[23554]
1995 Apr 7.99
3645 days
2005 Mar 30
Cylinder
1815
10.1 long
3.05 dia
1995 Apr 8.28
2005 Mar 30.19
26.45
25.93
D
Progress-M 27 *
[Soyuz-U]
1995-20 A
[23555]
BAI
1995 Apr 9.82
43.32 days
1995 May 23.14
Cyl+ 2 panels+ 7.9 long
1995 Apr 10.18
beehive+sphere 2.72 maxdia 1995 Apr 12.05
7250
1995 May 22.91
1995 May 23.87?
51.64
51.65
51.65
51.64
89.60
92.40
92.50
92.50
6663
6771
6776
6776
230
388
394
396
279
396
400
399
0.004
0.0006
0.0005
0.0002
118
0
345
347
D
Soyuz-U 3rd stage
(Block I)
1995-20 B
[23556]
1995 Apr 9.82
2 days
1995 Apr 11
Cylinder
2400
8.1 long
2.66 dia
1995 Apr 10.18
1995 Apr 11.52
51.63
51.64
88.45 6577
87.47 6528
187
146
209
152
0.002
0.0005
82
95
D
Fragments
1995-20 C
[23583]
1996 Jun 25
443 days
1995-20 D
[23588]
1997 Mar 19
709 days
1995
1995
1995
1997
May
Jun
May
Feb
23.83
24.72
25.48
15.24
51.65
51.62
51.64
51.66
92.52
87.98
92.50
89.40
6776
6553
6775
6623
394
168
393
243
402
180
400
246
0.0006
0.0009
0.0005
0.0002
15
203
353
114
ERS 2
[Ariane 40]
(#42)
1995-21 A
[23560]
KOU-ELA2
1995 Apr 21.07
Box+ panel
+ panel +
SAR antenna
2516
11.8 high
2.4x11.7
1x10
1995
1995
1995
2010
Apr
Apr
Apr
Dec
21.08
21.78
22.19
25.14
98.56
98.55
98.55
98.55
100.55
100.52
100.42
100.53
7163
7162
7157
7162
783
782
774
783
786
784
784
784
0.0002
0.0001
0.0007
0.00009
37
168
149
81
Ariane-4 3rd stage
(H 10+) + VEB
1995-21 B
[23561]
1995 Apr 21.07
Cylinder
1250
Cylinder
530
11.7 long
2.6 dia
1 high
4 dia
1995 Apr 21.43
2010 Dec 23.89
98.48
98.51
100.47 7159
100.23 7148
775
764
786
775
0.0008
0.0008
240
80
Fragments
1995-21 C-H
6 pieces, 1 has decayed
Docked with MIR (front port) 1995 Apr 11.88; undocked 1995 May 22.99
26569
31493
40202
42157
42165
42165
Apogee
height
(km)
1995-19 A
[23553]
CC
*
718.32
927.00
1337.00
1435.68
1436.10
1436.08
Perigee
height
(km)
AMSC 1
[Atlas-2A]
D
Apr
Apr
Apr
Apr
May
Dec
Nodal
period
(min)
716.90 26534
89.53 6630
For orbital information see extra pages at end of year
RAE Table of Earth Satellites (extended)
(Compiled 2006)
Page 1995-11
Cospar ID
[Norad #] Launchsite
Cospar ID
Launchdate
Lifetime + Descent date
[Norad]
Shape and
weight (kg)
Descent date
Semi
major axis
(km)
USA 110
[Titan-4]
1995-22 A
[23567]
CC
1995 May 14.57
> million years?
4500?
Titan-4 3rd stage
(Centaur)
1995-22 B
[23568]
1995 May 14.57
> million years?
2700?
Intelsat 706
[Ariane-44LP]
(#43)
1995-23 A
[23571]
KOU-ELA2
1995 May 17.27
> million years
Box+ 2 panels
4180
2.45x2.20
x4.7
27.2 span
1995
1995
1995
1995
1995
1995
2010
17.51
18.68
19.87
22.48
23.80
10.84
22.80
7.06
3.97
0.44
0.07
0.04
0.02
0.02
D
Ariane-4 3rd stage
(H-10-3)
+ VEB
1995-23 B
[23572]
1995 May 17.27
180 days
1995 Nov 13
Cylinder
1250
Cylinder
530
10.2 long
2.6 dia
1 high
4 dia
1995 May 18.84
1995 Sep 5.01
7.23
7.32
D
Spektr *
[Proton-K]
1995-24 A
[23579]
BAI
1995 May 20.15
2134 days
2001 Mar 23
Cylinder
19640
13 long
1995 May
4.35 maxdia 1995 May
1995 May
1995 May
1995 May
1995 Jun
2000 Dec
D
Proton-K 3rd stage
1995-24 B
[23580]
1995 May 20.15
20 days
1995 Jun 9
Cylinder
4185
4 long
4.1 dia
*
Docked with MIR (front port) 1995 Jun 1.04; relocated to sideport 1995 Jun 1.7-1.8; de-orbited with MIR over Pacific Ocean.
Year of Launch 1995
Name
[Launcher]
Fragments
Size
(m)
Lifetime
Date of
orbital
determination
Orbital
Inclination
(deg)
Nodal
period
(min)
Perigee
height
(km)
Apogee
height
(km)
Orbital
Argument
eccentricity of perigee
(deg)
173
4379
22014
35732
35735
35784
35772
35810
35798
35778
35919
35837
35789
35800
0.731
0.594
0.195
0.002
0.001
0.00006
0.0003
179
179
178
52
51
47
231
112
75
36216
27191
0.736
0.678
181
301
Geosynchronous orbit? No TLE issued.
Geosynchronous orbit? No TLE issued.
May
May
May
May
Jun
Jul
Dec
631.03
714.18
1098.88
1438.10
1436.08
1436.10
1436.10
24371
26467
35275
42204
42165
42165
42165
637.73 24543
469.53 20011
20.83
21.39
25.16
29.16
31.19
1.85
14.79
51.66
51.66
51.65
51.65
51.65
51.65
51.64
89.82
90.55
91.38
91.73
91.95
92.48
90.93
6644
6680
6721
6738
6749
6775
6693
215
262
312
335
355
393
310
315
341
372
384
386
400
331
0.008
0.006
0.004
0.004
0.002
0.0005
0.002
84
103
61
112
108
33
112
1995 May 20.57
1995 Jun 9.40
51.67
61.64
89.62 6634
87.07 6508
213
125
298
133
0.006
0.0007
79
262
RAE Table of Earth Satellites (extended)
(Compiled 2006)
Page 1995-12
Launchdate
Lifetime + Descent date
[Norad]
Shape and
weight (kg)
Descent date
Size
(m)
Lifetime
Semi
major axis
(km)
Year of Launch 1995
Name
[Launcher]
Fragments
Cospar ID
[Norad #] Launchsite
Cospar ID
Date of
orbital
determination
GOES 9
[Atlas-1]
1995-25 A
[23581]
CC
1995 May 23.24
> million years
Box+ panel +
boom + panel
2105
2.4x2.6x2.6 1995 May
27 span
1995 May
1995 Jun
1995 Jun
1995 Jul
1995 Sep
2010 Dec
D
Atlas-1 2nd stage
(Centaur)
1995-25 B
[23582]
1995 May 23.24
174 days
1995 Nov 13
Cylinder
1725
9.15 long
3.05 dia
D
Cosmos 2312
[Molniya-M]
1995-26 A
[23584]
PLE
1995 May 24.84
6697 days
2013 Sep 23
D
Molniya-M 3rd stage 1995-26 B
(Block I)
[23585]
D
Orbital
Inclination
(deg)
Nodal
period
(min)
Orbital
Argument
eccentricity of perigee
(deg)
144
35621
35633
35773
35782
35780
36193
42013
42408
35886
35800
35785
35792
36213
0.762
0.075
0.003
0.0003
0.00004
0.0001
0.0002
180
94
101
250
215
276
347
27.08
0.28
0.29
0.25
0.47
0.40
6.65
1995 May 24.04
1995 Oct 19.48
27.12
27.04
748.67 27312
660.92 25134
126
142
41741
37369
0.762
0.741
180
265
Drum+ 2 panels 2 long
1900
2 dia
1995
1995
1995
2010
2013
24.89
27.35
27.85
24.68
23.36
62.90
62.89
62.91
65.47
61.95
708.12
717.65
717.73
717.13
91.95
602
603
608
1474
74
39274
39744
39744
38848
666
0.735
0.737
0.737
0.704
0.044
318
318
318
206
215
1995 May 24.84
76 days
1995 Aug 8
Cylinder
2000
1995 May 25.21
1995 Jul 1.55
1995 Aug 7.88
62.81
62.81
62.79
92.50 6775
91.20 6712
87.68 6539
213
208
148
581
459
172
0.027
0.019
0.002
119
124
135
Molniya-M 4th stage 1995-26 C
Casing
[23586]
1995 May 24.84
29 days
1995 Jun 22
Hollow cyl
330
1995 May 25.21
1995 Jun 8.24
1995 Jun 22.28
62.84
62.85
62.84
92.45 6773
91.02 6703
87.18 6514
180
176
119
608
474
150
0.032
0.022
0.002
121
123
113
Molniya-M 4th stage 1995-26 D
[23587]
1995 May 24.84
Cylinder
900
2.5 long
2.2 dia
1995 May 27.16
2010 Dec 23.21
62.99
67.07
708.27 26321
708.22 26319
703
1851
39181
38030
0.731
0.687
318
182
UFO 5 (USA 111)
[Atlas-2]
1995-27 A
[23589]
CC
1995 May 31.64
> million years
Box+ 2 panels
+ antennae
3000
2.7x2.2x2.6
3.6 to
6.8 high
26.5 span
1995
1995
1995
1995
1995
1995
1997
31.73
4.43
7.64
10.29
11.00
28.00
30.74
26.97
13.39
5.08
5.09
5.05
5.02
4.09
290
8300
35096
35060
35748
35768
35775
26522
36510
36520
36519
36532
35805
35801
0.663
0.490
0.017
0.017
0.009
0.0004
0.0003
171
168
145
145
146
134
294
Atlas-2 2nd stage
(Centaur)
1995-27 B
[23590]
1995 May 31.64
Cylinder
1815
10.1 long
3.05 dia
1995 Jun 1.48
2010 Dec 24.74
27.03
26.74
291
283
26445
22679
0.662
0.627
173
164
8.1 long
2.66 dia
May
Jun
Jun
Jun
Jul
Jul
Dec
461.57
810.00
1437.20
1436.27
1454.22
1436.10
1436.18
27457
45393
42138
42165
42162
42165
42582
Apogee
height
(km)
24.57
29.33
2.70
19.18
28.20
5.73
23.44
May
May
May
Dec
sep
754.63
1544.15
1434.73
1436.10
1435.97
1436.08
1457.43
Perigee
height
(km)
26317
26552
26555
26540
6749
19784
28784
42186
42168
42519
42165
42166
460.27 19747
395.87 17860
RAE Table of Earth Satellites (extended)
(Compiled 2006)
Page 1995-13
Launchdate
Lifetime + Descent date
[Norad]
Shape and
weight (kg)
Descent date
Size
(m)
Lifetime
Date of
orbital
determination
Orbital
Inclination
(deg)
Semi
major axis
(km)
Year of Launch 1995
Name
[Launcher]
Fragments
Cospar ID
[Norad #] Launchsite
Cospar ID
Nodal
period
(min)
Perigee
height
(km)
Apogee
height
(km)
Orbital
Argument
eccentricity of perigee
(deg)
D
Cosmos 2313
[Tsyklon-M]
1995-28 A
[23596]
BAI
1995 Jun 8.20
764 days
1997 Jul 11
Cylindrical
+ stubby cyl
6 long
2 dia
1.5 long
3 dia
1995 Jun 8.32
1995 Jun 8.83
1997 Jul 11.78
65.04
65.04
65.00
92.87 6793
92.77 6789
87.60 6534
399
403
139
430
417
172
0.002
0.001
0.002
284
263
260
D
Tsyklon-M 2nd stage 1995-28 B
[23597]
1995 Jun 8.20
1 day
1995 Jun 9
Cylinder
4000
10.9 long
3 dia
1995 Jun 8.31
1995 Jun 8.68
65.01
65.01
89.38 6623
88.18 6563
114
108
374
261
0.020
0.012
51
55
D
Fragments
12 pieces, all have decayed
D
For orbital information see extra pages at end of year
DirecTV 3
1995-29 A
(DBS 3 / Nimiq 3) [23598]
[Ariane-42P] (#44) KOU-ELA2
1995 Jun 10.02
> million years
Box+ 2 panels
2934 full
1259 empty
2.8x3.5x4.3 1995 Jun 10.61
to 5.1 high 1995 Jun 11.90
26.5 span
1995 Jun 14.70
1995 Jun 16.60
1995 Jun 17.87
1995 Jul 1.44
2010 Dec 22.39
7.04
7.05
0.80
0.05
0.08
0.01
1.65
Ariane-4 3rd stage
(H-10-3)
+ VEB
1995-29 B
[23599]
1995 Jun 10.02
4600 days
2008 Jan 13
Cylinder
1250
Cylinder
530
10.2 long
2.6 dia
1 high
4 dia
1995 Jun 11.03
2008 Jan 13.30
7.14
6.76
1995-30 A
[23600]
CC-LC39
1995 Jun 27.81
10.81 days
1995 Jul 7.62
Delta wing
97387
37.3 long
5.5 dia
23.8 span
1995
1995
1995
1995
1995
1995
1995
1995
51.65
51.64
51.65
51.65
51.64
51.65
51.65
51.65
D STS-071 *
7M Atlantis F14
R [Shuttle]
*
1995-28 C-P
Jun
Jun
Jun
Jun
Jun
Jul
Jul
Jul
27.87
27.97
28.45
29.40
29.69
4.25
4.52
7.58
550.53
632.03
1144.50
1389.70
1436.93
1436.08
1454.50
22251
24396
36244
41252
42181
42165
42524
574.30 22887
88.62 6584
88.58
91.37
91.47
92.45
92.47
92.47
92.43
88.93
6583
6720
6725
6773
6774
6774
6772
6600
220
223
23905
33914
35775
35780
36144
31525
35813
35826
35833
35830
35792
36148
0.703
0.729
0.164
0.023
0.0007
0.0002
0.00005
178
179
182
159
337
331
285
216
118
32801
293
0.712
0.013
179
339
106
294
302
389
392
393
390
48
302
389
390
399
399
398
397
396
0.015
0.007
0.007
0.0007
0.0005
0.0003
0.0005
0.026
20
184
181
151
133
168
174
6
Crew of 5 astronauts (Gibson, Precourt, Baker, Harbaugh and Dunbar) and 2 cosmonauts (Solovyov and Budarin) docked with MIR (Kristall port) 1995 Jun 29.54
Undocked 1995 Jul 4.47 with the 5 astronauts and the crew of Soyuz-TM 21 (Dezhurov, Strekalov and Thagard) and landed at KSC.
Cosmonauts Solovyov and Budarin remained aboard MIR and returned 1995 Sep 11.29 with Soyuz-TM 21 (1995-10 A).
Shuttle carried docking adapter for docking with Kristall module.
RAE Table of Earth Satellites (extended)
(Compiled 2006)
Page 1995-14
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)
6500
7 long
2.5 dia
1995
1995
1995
1995
1995
1995
1995
1995
1995
1995
1995
1995
1995
1995
1995
1995
28.88
2.86
3.92
10.89
11.14
25.87
26.55
30.59
31.27
6.85
7.17
8.23
8.85
26.41
26.79
6.81
67.13
67.13
67.13
67.13
67.13
67.13
67.13
67.12
67.12
67.12
67.12
67.12
67.12
67.12
67.12
67.12
89.60
89.38
89.68
89.47
90.23
89.42
89.50
89.23
89.55
89.17
89.90
89.85
90.33
89.60
89.90
89.40
Year of Launch 1995
Name
[Launcher]
Fragments
D
D
Cospar ID
[Norad #] Launchsite
Cospar ID
Perigee
height
(km)
Apogee
height
(km)
Orbital
Argument
eccentricity of perigee
(deg)
6633
6623
6637
6626
6664
6624
6628
6615
6631
6612
6648
6646
6669
6633
6648
6624
166
163
168
167
167
160
160
158
167
163
169
169
177
171
180
174
343
325
350
329
404
332
339
315
338
304
369
365
405
337
358
315
0.013
0.012
0.014
0.012
0.018
0.013
0.013
0.012
0.013
0.011
0.015
0.015
0.017
0.013
0.013
0.011
94
90
80
77
81
67
68
64
99
91
105
105
113
93
134
124
Cosmos 2314
[Soyuz-U]
1995-31 A
[23601]
PLE
1995 Jun 28.77
70 days
1995 Sep 6.8
Soyuz-U 3rd stage
(Block I)
1995-31 B
[23602]
1995 Jun 28.77
6 days
1995 Jul 4
Cylinder
2400
8.1 long
2.66 dia
1995 Jun 28.88
1995 Jul 4.13
67.13
67.13
89.52 6630
86.90 6499
165
110
336
131
0.013
0.002
95
110
Cosmos 2315
[Kosmos-3M]
1995-32 A
[23603]
PLE
1995 Jul 5.13
Cylinder
+ gavity boom
825
2.1 long
2 dia
1995 Jul 5.19
2010 Dec 25.12
82.91
82.90
104.93 7370
104.90 7368
969
966
1013
1013
0.003
0.003
282
76
Kosmos-3M 2nd stage 1995-32 B
[23604]
1995 Jul 5.13
Cylinder
1434
4.21 long
2.4 to
3.2 maxdia
1995 Jul 5.26
2010 Dec 24.93
82.90
82.90
104.82 7364
104.78 7363
971
967
1001
1002
0.002
0.002
277
348
Helios 1A
[Ariane 40]
(#45)
1995 Jul 7.68
7048
7052
7059
665
672
679
675
676
681
0.0008
0.0003
0.0001
187
127
153
7059
7059
680
678
681
683
0.0001
0.0004
106
116
CERISE *
UPM/LBSAT 1
1995-33 A
[23605]
KOU-ELA2
2537
1995-33 B
[23606]
1995 Jul 7.68
1995-33 C
[23607]
1995 Jul 7.68
Jun
Jul
Jul
Jul
Jul
Jul
Jul
Jul
Jul
Aug
Aug
Aug
Aug
Aug
Aug
Sep
Nodal
period
(min)
1995 Jul 7.89
98.07
98.15
1995 Jul 8.17
98.07
98.23
2009 Dec 8.63
98.10
98.37
Orbit from amateur observations.
2010 Apr 17.03
98.14
98.37
2010 Sep 8.05
98.11
98.37
50
1995 Jul 9.21
2010 Dec 12.63
98.07
98.31
98.15 7048
96.95 6991
665
607
675
618
0.0007
0.0008
183
108
47
1995 Jul 8.92
2010 Dec 24.81
98.07
98.18
98.15 7049
97.62 7024
666
641
675
649
0.0006
0.0005
181
284
1995 33 continued on next page
*
Cerise, 1995-33B and Spot 1 debris, 1986-19 RF, collided 1996 Jul 24.408, see info in extra pages at the end of the year.
RAE Table of Earth Satellites (extended)
(Compiled 2006)
Page 1995-15
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)
Cylinder
1250
Cylinder
530
10.2 long
2.6 dia
1 high
4 dia
1995 Jul 8.17
2010 dec 24.89
98.04
98.26
1996 Jul 27.42
2010 Dec 24.87
98.10
98.31
Year of Launch 1995
Name
[Launcher]
Fragments
Cospar ID
[Norad #] Launchsite
Cospar ID
Nodal
period
(min)
Perigee
height
(km)
Apogee
height
(km)
Orbital
Argument
eccentricity of perigee
(deg)
98.15 7046
96.85 6986
649
592
686
623
0.003
0.002
214
79
98.13 7048
96.07 6948
663
566
676
573
0.0009
0.0005
62
267
185
1300
185
39200
299
286
285
333
315
314
0.003
0.002
0.002
193
149
242
35792
35759
35757
35578
35787
35782
35657
35804
35852
35813
35639
35790
35790
35915
0.0001
0.001
0.0007
0.0007
0.00003
0.00009
0.003
354
300
260
237
221
128
322
305
334
35753
33343
0.726
0.711
0
104
35695
35664
35756
35774
0.0007
0.001
170
0
Ariane-4 3rd stage
[H-10-3]
+ VEB
1995-33 D
[23608]
1995 Jul 7.68
Cerise fragment
1995-33 E
[23994]
USA 112
[Titan-4]
1995-34 A
[23609]
CC
1995 Jul 10.51
> million years
8000
Titan-4 3rd stage
(Centaur)
1995-34 B
[23610]
1995 Jul 10.51
> million years
Cylinder
2700
9.0 long
4.1 dia
Orbit similar to 1995-34 A
1995-35 A
[23612]
CC-LC39
1995 Jul 13.57
8.93 days
1995 Jul 22.50
Delta wing
88540
37.3 long
5.5 dia
23.8 span
1995 Jul 13.84
1995 Jul 14.80
1995 Jul 22.30
28.46
28.46
28.46
TDRS 7
1995-35 B
[23613]
1995 Jul 13.57
> million years
Hexagonal
body
+ 2 panels
+ 2 antennae
2 across
6 high
17.4 span
1995
1995
1995
1995
1995
1995
2010
14.10
14.22
14.48
19.25
3.30
20.40
24.59
0.01
0.04
0.04
0.02
0.01
0.05
12.16
IUS lower part
1995-35 C
[23614]
1995 Jul 13.57
Cylinder
1157
3.52 long
2.34 dia
1995 Jul 14.75
2010 Dec 24.62
26.31
26.06
632.48 24408
586.77 23217
IUS upper part
1995-35 D
[23615]
1995 Jul 13.57
> million years
Cylinder
1085
2.1 long
1.61 dia
1995 Jul 31.04
2010 Dec 24.70
2.06
14.10
1433.00 42104
1432.67 42098
D
Progress-M 28 *
[Soyuz-U]
1995-36 A
[23617]
BAI
1995 Jul 20.13
46.24 days
1995 Sep 4.374
Cyl+ 2 panels+ 7.9 long
1995 Jul 20.31
beehive+sphere 2.72 maxdia 1995 Jul 22.13
7250
1995 Jul 22.24
1995 Sep 4.07
51.64
51.64
51.65
51.65
89.78
90.95
92.47
92.45
6642
6700
6774
6773
241
292
393
392
287
351
398
397
0.003
0.004
0.0003
0.0004
139
310
259
54
D
Soyuz-U 3rd stage
(Block I)
1995-36 B
[23618]
1995 Jul 20.13
3 days
1995 Jul 23
Cylinder
2400
51.60
51.63
88.62 6585
87.23 6516
187
132
225
142
0.003
0.0008
94
75
#
$
*
Estimated transfer orbit.
Crew of 5 astronauts (Henricks, Kregel, Thomas, Currie and Weber)
Progress-M 28 docked 1995 Jul 22.194 with MIR (front port; undocked 1995 Sep 4.215
D STS-070 $
5M Discovery F21
R [Shuttle]
57
1995 Jul 31
64
Geosynchronous orbit?
8.1 long
2.66 dia
Jul
Jul
Jul
Jul
Aug
Aug
Dec
1995 Jul 20.30
1995 Jul 23.06
720
90.85 6695
90.53 6679
90.52 6678
1436.68
1437.08
1436.05
1427.00
1436.20
1436.10
1436.08
42176
42184
42164
41987
42167
42165
42165
270#
RAE Table of Earth Satellites (extended)
(Compiled 2006)
Page 1995-16
Launchdate
Lifetime + Descent date
[Norad]
Shape and
weight (kg)
Descent date
Semi
major axis
(km)
Year of Launch 1995
Name
[Launcher]
Fragments
Cospar ID
[Norad #] Launchsite
Cospar ID
Size
(m)
Lifetime
Date of
orbital
determination
Orbital
Inclination
(deg)
Nodal
period
(min)
Perigee
height
(km)
Apogee
height
(km)
Orbital
Argument
eccentricity of perigee
(deg)
Cosmos 2316
(Glonass 74)
[Proton-K]
1995-37 A
[23620]
BAI
1995 Jul 24.66
1 million years
Cylindrical
+ 2 panels
1300
1995
1995
1995
2010
Jul
Aug
Aug
Dec
25.14
2.09
15.55
23.15
64.86
64.85
64.84
66.45
675.25
668.45
675.72
675.73
25496
25325
25508
25508
19101
18765
19081
19095
19134
19127
19177
19164
0.0007
0.007
0.002
0.001
217
247
173
177
Cosmos 2317
(Glonass 75)
1995-37 B
[23621]
1995 Jul 24.66
1 million years
Cylindrical
+ 2 panels
1300
1995
1995
1995
1995
1995
1995
1995
2010
Jul
Jul
Jul
Aug
Aug
Aug
Aug
Dec
24.67
25.14
28.42
3.99
6.34
8.22
15.26
24.27
64.87
64.75
64.85
64.86
64.87
64.89
64.85
66.46
675.55
675.70
675.25
677.53
676.25
675.73
675.72
675.73
25504
25507
25496
25555
25521
25508
25508
25508
19106
19056
19104
19119
19101
19084
19084
19099
19145
19202
19131
19223
19184
19175
19175
19160
0.0008
0.003
0.0005
0.002
0.002
0.002
0.002
0.001
193
356
226
133
168
184
185
180
Cosmos 2318
(Glonass 76)
1995-37 C
[23622]
1995 Jul 24.66
1 million years
Cylindrical
+ 2 panels
1300
1995
1995
1995
1995
1995
1995
1995
2010
Jul
Jul
Aug
Aug
Aug
Aug
Aug
Dec
25.14
31.71
2.13
5.93
6.40
9.22
16.26
24.33
64.84
64.85
64.86
64.67
64.86
64.85
64.85
66.45
675.37
681.55
984.03
676.53
678.02
675.73
675.72
675.73
25499
25654
25717
25528
25566
25508
25508
25508
19110
19139
19146
19037
19110
19037
19036
19072
19131
19413
19530
19263
19264
19223
19222
19187
0.0004
0.005
0.007
0.004
0.003
0.004
0.004
0.002
211
72
83
141
131
168
168
137
D
Proton-K 3rd stage
1995-37 D
[23623]
1995 Jul 24.66
>1 day
1995 Jul 25
Cylinder
4185
4 long
4.1 dia
1995 Jul 24.84
1995 Jul 25.21
64.85
64.85
87.60 6534
87.13 6511
148
127
152
138
0.001
0.0008
328
271
D
Proton-K 4th stage
casing
1995-37 E
[23624]
1995 Jul 24.66
>1 day
1995 Jul 25
Hollow cyl
800
4.0 long
3.7 dia
1995 Jul 24.84
1995 Jul 24.90
64.83
64.82
87.32 6520
87.50 6530
138
146
146
156
0.0006
0.0007
47
77
Proton-K 4th stage
(Block DM)
1995-37 F
[23625]
1995 Jul 24.66
1 million years
Cylinder
2350
6.22 long
3.7 dia
1995 Jul 25.14
2010 Dec 24.24
64.85
66.45
674.72 25483
674.72 25483
19082
19087
19125
19120
0.0008
0.0006
250
210
D
Ullage motor
1995-37 J
[23630]
1995 Jul 24.66
2230 days
2001 Aug 31
Cylinder
55
0.90 long
0.68 dia
1995 Aug 2.22
2001 Aug 31.72
64.81
63.94
340.17 16142
87.80 6544
402
74
19125
257
0.580
0.014
297
216
D
Ullage motor
1995-37 K
[23631]
1995 Jul 24.66
2293 days
2001 Nov 2
Cylinder
55
0.90 long
0.68 dia
1995 Aug 2.22
2001 Nov 2.55
64.88
63.75
340.18 16143
89.52 6629
404
136
19124
365
0.580
0.017
297
201
D
Fragments
1995-37 G-H
2 pieces, both have decayed
For orbital information see extra pages at end of year
RAE Table of Earth Satellites (extended)
(Compiled 2006)
Page 1995-17
Launchdate
Lifetime + Descent date
[Norad]
Shape and
weight (kg)
Descent date
Size
(m)
Lifetime
Date of
orbital
determination
Semi
major axis
(km)
Orbital
Argument
eccentricity of perigee
(deg)
Year of Launch 1995
Name
[Launcher]
Fragments
Cospar ID
[Norad #] Launchsite
Cospar ID
DSCS-3B 4
[Atlas-2A]
1995-38 A
[23628]
CC
1995 Jul 31.98
> million years
Cylinder
1040
1.93 dia
2.06 high
No TLE available.
Atlas-2A 2nd stage
(Centaur 118)
1995-38 B
[23629]
1995 Jul 31.98
Cylinder
1815
10.1 long
3.05 dia
No TLE available.
IABS
+ adapter
1995-38 C
[23648]
1995 Jul 31.98
> million years
Cylindrical
227 + 45
2.9 dia
0.686 high
No TLE available.
Interball 1
[Molniya-M]
1995-39 A
[23632]
PLE
1995 Aug 3.00
1901 days
2000 Oct 16
1250
D
Molniya-M 3rd stage 1995-39 B
(Block I)
[23633]
1995 Aug 3.00
255 days
1996 Apr 14
Cylinder
1976
D
Molniya-M 4th stage 1995-39 C
Casing
[23634]
1995 Aug 3.00
113 days
1995 Nov 24
Hollow cyl
328.7
D
Molniya-M 4th stage 1995-39 D
(Block-2DL-SM2)
[23635]
1995 Aug 3.00
1928 days
2000 Nov 13
Cylinder
896.7
MAGION 4 (C-2T)
1995-39 F
[23646]
1995 Aug 3.00
Fragment
1995-39 E
D
D
Orbital
Inclination
(deg)
Nodal
period
(min)
1995 Aug 3.05
2000 Oct 16.58
63.81
66.22
1995 Aug 3.12
1996 Apr 4.62
62.83
62.80
94.60 6878
88.53 6580
1995 Aug 3.12
1995 Nov 24.64
62.81
62.78
94.75 6885
86.92 6500
2.5 long
2.2 dia
1995 Aug 3.05
2000 Nov 7.21
63.82
66.03
24 faced
spheroid
+ panels
0.53 dia
1995 Aug 3.39
1997 Apr 9.00
63.27
7034
[23638]
1995 Aug 21
18 days
1995 Aug 4.50
1995 Aug 20.83
62.79
62.81
PAS 4 (Intelsat 4) 1995-40 A
[Ariane 42L]
[23636]
(#46)
KOU-ELA2
1995 Aug 4.00
> million years
Box+ 2 panels
3043
3.53x2.84
x3.6
26.2 span
1995
1995
1995
1995
1995
1995
1995
2010
4.08
5.24
6.93
10.92
21.25
22.75
5.75
24.10
4.18
1.30
0.39
0.02
0.10
0.06
0.08
0.78
Ariane-4 3rd stage
(H-10-3)
+ VEB
1995 Aug 4.00
Cylinder
1250
Cylinder
530
10.2 long
2.6 dia
1 high
4 dia
1995 Aug 3.98
2010 Dec 24.08
4.17
4.03
1995-40 B
[23637]
8.1 long
2.66 dia
Aug
Aug
Aug
Aug
Sep
Sep
Oct
Dec
Perigee
height
(km)
5459.53 102706 509
5452.15 102614 -78
Apogee
height
(km)
192146 0.933
192548 0.939
315
6
233
182
765
221
0.039
0.003
112
146
205
96
807
147
0.044
0.004
112
344
5498.48 103194 505
5394.90 101894 -9
193126 0.933
191040 0.937
315
6
5454.22 102640 760
5453.95 102636 17067
191762 0.930
175448 0.772
314
329
228
172
791
254
0.041
0.006
112
125
507
10736
26461
35734
35720
35776
35774
36585
35735
35712
35729
35840
35789
35795
35798
36798
0.719
0.422
0.124
0.001
0.0008
0.0002
0.0003
0.002
179
180
164
33
24
345
22
103
517
620
36917
36870
0.725
0.721
179
254
94.82 6888
88.77 6592
636.05
844.78
1203.22
1436.13
1434.47
1436.05
1436.08
1482.60
24500
29602
37473
42165
42133
42164
42165
43070
659.40 25096
658.73 25079
RAE Table of Earth Satellites (extended)
(Compiled 2006)
Page 1995-18
Launchdate
Lifetime + Descent date
[Norad]
Shape and
weight (kg)
Descent date
Size
(m)
Lifetime
Date of
orbital
determination
Orbital
Inclination
(deg)
Semi
major axis
(km)
Year of Launch 1995
Name
[Launcher]
Fragments
D
Cospar ID
[Norad #] Launchsite
Cospar ID
532.35
1073.53
1122.07
1280.43
1353.08
1429.70
1436.13
1444.75
21578
34730
35769
39060
40524
42040
42165
42334
Perigee
height
(km)
Apogee
height
(km)
Orbital
Argument
eccentricity of perigee
(deg)
1373
26886
27963
31841
33220
35529
35779
35951
29386
29817
30818
33522
35071
35794
35795
35960
0.644
0.042
0.040
0.022
0.023
0.003
0.0002
0.0001
359
199
204
179
217
274
84
51
Mugunghwa 1
(Koreasat 1)
[Delta-2 (7925)]
1995-41 A
[23639]
CC
1995 Aug 5.47
> million years
Box+ 2 panels
1459
1.63x1.32
x0.99
15.45 span
1995
1995
1995
1995
1995
1995
1995
2010
5.89
10.65
17.72
19.92
24.78
28.38
16.63
23.83
20.55
0.20
0.22
0.11
0.07
0.28
0.05
10.21
Delta-2 2nd stage
1995-41 B
[23640]
1995 Aug 5.47
Cylinder
919
5.88 long
2.44 dia
1995 Aug 5.89
2010 Dec 24.91
26.67
26.68
108.47 7534
108.43 7533
938
936
1373
1372
0.029
0.0029
216
18
Delta-2 3rd stage
PAM-D AKM
1995-41 C
[23641]
1995 Aug 5.47
Cone-cyl
205
2.29 long
1.5 dia
1995 Aug 5.89
2010 Dec 25.92
20.61
20.75
532.45 21761
532.53 21764
1367
1407
29398
29363
0.644
0.642
359
190
Fragment
1995-41 D
[24310]
2003 Jun 14
2870 days
1996 Sep 16.49
2003 Jun 12.35
26.68
26.62
108.55 7538
92.88 6795
917
390
1402
442
0.032
0.004
12
227
Molniya-3 47
[Molniya-M]
Aug
Aug
Aug
Aug
Aug
Aug
Sep
Dec
Nodal
period
(min)
1995-42 A
[23642]
PLE
1995 Aug 9.10
Cylindrical
+ 6 panels
1750
3.6 long
1.6 dia
1995 Aug 9.15
1995 Aug 16.75
2010 Dec 23.92
62.81
62.81
62.70
734.57 26968
718.53 26574
717.85 26558
414
425
438
40765
39966
39919
0.748
0.744
0.743
280
280
256
D
Molniya-M 3rd stage 1995-42 B
(Block I)
[23643]
1995 Aug 9.10
27 days
1995 Sep 5
Cylinder
2000
8.1 long
2.66 dia
1995 Aug 9.21
1995 Sep 5.36
62.82
62.82
90.55 6680
87.52 6530
208
139
394
164
0.014
0.002
136
165
D
Molniya-M 4th stage 1995-42 C
Casing
[23644]
1995 Aug 9.10
14 days
1995 Aug 25
Hollow cyl
330
1995 Aug 9.21
1995 Aug 25.30
62.82
62.79
90.93 6699
87.42 6525
180
132
460
161
0.021
0.002
126
114
Molniya-M 4th stage 1995-42 D
(Block ML)
[23645]
1995 Aug 9.10
Cylinder
900
1995 Aug 9.15
2010 Dec 23.99
62.79
63.39
735.67 26995
735.03 26980
431
524
40802
40678
0.748
0.744
280
251
2.5 long
2.2 dia
RAE Table of Earth Satellites (extended)
(Compiled 2006)
Page 1995-19
Launchdate
Lifetime + Descent date
[Norad]
Shape and
weight (kg)
Descent date
Size
(m)
Lifetime
Semi
major axis
(km)
1995 Aug 29.04
> million years
Box+2 panels
1820
2.7x2.2x2.6 1995 Aug 29.65
3.6 high
1995 Sep 10.38
35.1 span
1995 Sep 12.63
1995 Sep 14.79
1995 Sep 17.78
1995 Sep 30.62
1995 Oct 1.68
1995 Nov 5.59
1995 Dec 22.63
2010 Dec 23.30
23.15
0.25
0.07
0.07
0.07
0.06
0.05
0.04
0.02
5.46
1681.63
1621.15
1486.70
1437.45
1436.60
1435.97
1436.02
1436.13
1436.10
1452.37
Atlas-2AS 2nd stage 1995-43 B
(Centaur 117)
[23658]
1995 Aug 29.04
167 days
1996 Feb 12
Cylinder
1835
10.1 long
3.05 dia
23.03
22.89
N-STAR a
[Ariane-44P]
(#47)
1995-44 A
[23651]
KOU-ELA2
1995 Aug 29.28
> million years
Box+2 panels
3410
2.4x2.2x6.3 1995 Aug
27.3 span
1995 Aug
1995 Aug
1995 Sep
1995 Sep
1995 Sep
2010 Dec
29.08
30.39
30.79
2.69
4.68
26.39
25.69
7.03
3.48
0.09
0.05
0.07
0.02
4.87
Ariane-4 3rd stage
(H-10-3)
+ VEB
1995-44 B
[23652]
1995 Aug 29.28
137 days
1996 Jan 13
Cylinder
1250
Cylinder
530
10.2 long
2.6 dia
1 high
4 dia
1995 Aug 29.80
1996 Jan 11.72
6.81
6.46
Cosmos 2319
[Proton-K]
1995-45 A
[23653]
BAI
1995 Aug 30.81
> million years
Box+2 panels
2300
1995
1995
1995
2010
31.65
10.69
13.76
16.97
1.48
1.26
1.56
11.03
D
Proton-K 3rd stage
1995-45 B
[23654]
1995 Aug 30.81
4 day
1995 Sep 4
Cylinder
4185
4.0 long
4.1 dia
1995 Aug 30.87
1995 sep 3.29
51.65
61.64
D
Proton-K 4th stage
casing
1995-45 C
[23655]
1995 Aug 30.81
>1 day
1995 Aug 31
Hollow cyl
800
4 long
3.7 dia
1995 Aug 30.87
1995 Aug 31.54
D
Proton-K 4th stage
(Block DM)
1995-45 D
[23656]
1995 Aug 30.81
1 million years
Cylinder
2350
6.22 long
3.7 dia
1995 Sep 2.58
2010 Dec 25.92
Year of Launch 1995
Name
[Launcher]
Fragments
Cospar ID
[Norad #] Launchsite
Cospar ID
JCSat 1
[Atlas-2AS]
D
D
1995-43 A
[23649]
CC
1995 45 continued on next page.
Date of
orbital
determination
1995 Nov 29.98
1995 Dec 28.38
Aug
Sep
Sep
dec
Orbital
Inclination
(deg)
Nodal
period
(min)
Perigee
height
(km)
Apogee
height
(km)
Orbital
Argument
eccentricity of perigee
(deg)
248
35718
35707
35704
35746
35740
35740
35781
35782
36035
80682
42951
37835
35921
35846
35828
35830
35793
35791
36173
0.859
0.079
0.025
0.003
0.001
0.001
0.001
0.0002
0.0001
0.002
180
167
125
52
46
9
8
89
269
282
1639.62 46060
1639.18 46052
219
169
79143
79178
0.857
0.858
202
209
630.27
774.13
1391.63
1431.18
1435.45
1436.12
1452.70
168
7344
34090
35599
35751
35775
36059
35777
35755
35732
35781
35796
35798
36162
0.731
0.509
0.020
0.002
0.0005
0.0003
0.001
178
179
169
256
274
267
230
130
112
37144
2890
0.740
0.176
178
20
35805
38741
35737
35771
35959
35835
35834
35783
0.002
0.001
0.001
0.0001
263
266
270
175
88.33 6571
87.05 6507
190
126
195
130
0.0004
0.0004
303
232
51.65
51.63
88.48 6578
87.75 6542
193
162
206
164
0.001
0.0002
68
87
1.57
11.06
1438.20 42206
1437.35 42189
35741
35729
35914
35893
0.002
0.002
297
263
46844
45713
43149
42191
42175
42162
42163
42166
42165
42483
24351
27928
41290
42069
42152
42165
42489
656.25 25016
116.00 7880
1441.02
1436.20
1436.05
1435.63
42261
42167
42164
42156
RAE Table of Earth Satellites (extended)
(Compiled 2006)
Page 1995-20
Launchdate
Lifetime + Descent date
[Norad]
Shape and
weight (kg)
Descent date
Size
(m)
Lifetime
Date of
orbital
determination
Orbital
Inclination
(deg)
Semi
major axis
(km)
Year of Launch 1995
Name
[Launcher]
Fragments
Cospar ID
[Norad #] Launchsite
Cospar ID
Nodal
period
(min)
Perigee
height
(km)
Apogee
height
(km)
Orbital
Argument
eccentricity of perigee
(deg)
D
Ullage motor
1995-45 E
[23660]
1995 Aug 30.81
280.8 days
1996 Jun 6.4
Cylinder
55
0.90 long
0.68 dia
1995 Aug 31.31
1996 Jun 6.43
47.49
46.62
634.53 24460
94.40 6868
283
96
35880
882
0.728
0.572
0
124
D
Ullage motor
1995-45 F
[23661]
1995 Aug 30.81
Cylinder
55
0.90 long
0.68 dia
1995 Aug 31.31
2002 May 7.58
47.53
46.52
635.45 24484
90.40 6672
338
116
35873
471
0.726
0.027
0
73
D
Fragments
1995-45 G
[23663]
1995 Sep 7
8 days
1995-45 H
[23664]
1995 Sep 2
3 days
1995 Sep 1.40
1996 Sep 6.21
1995 Sep 2.30
51.60
51.60
51.68
91.73 6738
90.35 6671
91.90 6746
191
184
191
527
400
544
0.025
0.017
0.026
89
99
94
Sich 1
{Tsyklon]
1995-46 A
[23657]
PLE
1995 Aug 31.28
Conical
1560
3 high
1.4 maxdia
1995 Aug 31.41
2010 Dec 24.74
82.52
82.53
97.72 7028
97.17 7002
631
607
668
639
0.003
0.002
276
337
FAISat Alfa
1995-46 B
[NNA]
1995 Aug 31.28
Cube
57
0.70x0.35
x0.35
Failed to separate from Sich 1
Tsyklon 3rd stage
1995-46 C
[23659]
1995 Aug 31.28
Cylinder
1000
2.7 long
2.2 dia
1995 Aug 31.55
2010 Dec 25.46
82.53
82.53
97.72 7028
97.48 7017
631
619
667
658
0.003
0.003
278
48
1995-47 A
[23665]
BAI
1995 Sep 3.38
179.07 days
1996 Feb 29.45
Cyl+ 2 panels+ 7.9 long
1995 Sep 3.43
beehive+sphere 2.72 maxdia 1995 Sep 3.88
7150
1995 Sep 5.42
1995 Sep 5.81
1996 Feb 28.07
51.62
51.65
51.65
51.65
51.65
88.63
89.70
89.73
92.45
92.43
6585
6638
6640
6773
6773
195
232
237
392
390
217
287
286
397
398
0.002
0.004
0.004
0.0004
0.00006
107
121
126
71
41
1995-47 B
[23666]
1995 Sep 3.38
3 days
1995 Sep 6
Cylinder
2400
51.64
51.62
88.55 6582
87.32 6520
195
139
211
143
0.001
0.0003
107
238
D
D Soyuz-TM 22 *
3M [Soyuz-U2]
R
D
Soyuz-U2 3rd stage
(Block I)
*
Crew of 2 cosmonauts (Gidzenko and Avdeyev) and ESA astronaut (Reiter) docked 1995 Sep 5.44 with MIR (front port); undocked 1996 Feb 29.31
8.1 long
2.66 dia
1995 Sep 3.43
1995 Sep 6.06
RAE Table of Earth Satellites (extended)
(Compiled 2006)
Page 1995-21
Launchdate
Lifetime + Descent date
[Norad]
Shape and
weight (kg)
Descent date
Size
(m)
Lifetime
Date of
orbital
determination
Orbital
Inclination
(deg)
Semi
major axis
(km)
Delta wing
99663
37.3 long
5.5 dia
23.8 span
1995
1995
1995
1995
1995
1995
1995
1995
28.47
28.47
28.47
28.46
28.47
28.47
28.47
28.46
91.98
92.02
92.55
92.55
92.53
91.37
91.37
91.37
1995 Sep 8.65
1995 Sep 9.60
Year of Launch 1995
Name
[Launcher]
Fragments
Cospar ID
[Norad #] Launchsite
Cospar ID
Orbital
Argument
eccentricity of perigee
(deg)
6751
6752
6778
6778
6777
6720
6720
6720
368
369
396
396
393
338
337
338
376
377
403
403
404
346
346
345
0.0006
0.00006
0.0005
0.0005
0.0008
0.0006
0.0007
0.0005
262
266
272
285
317
277
288
337
28.47
28.46
91.98 6751
91.98 6750
368
368
376
376
0.0006
0.0006
273
288
92.58 6780
92.57 6779
396
396
407
404
0.0008
0.0006
176
306
273
4744
11749
35014
35514
35726
35753
35747
35746
35762
35754
35738
35714
35729
35729
35826
35829
35826
35826
35798
0.727
0.582
0.398
0.009
0.003
0.001
0.0009
0.0009
0.0009
0.0004
179
180
178
139
104
139
126
132
131
230
372
370
36875
36143
0.730
0.726
180
135
1995 Sep 7.63
10.86 days
1995 Sep 18.49
D
R
Spartan 201-03 %
1995-48 B
[23668]
1995 Sep 7.63
10.86 days
1995 Sep 18.49
D
R
Wake Shield &
Faculity 2
1995-48 C
[23669]
1995 Sep 7.63
10.86 days
1995 Sep 18.49
Disk
1979
3.7 dia
1995 Sep 11.67
1995 Sep 14.33
28.48
28.47
Telstar 402R *
[Ariane-42L]
(#48)
1995-49 A
[23670]
KOU-ELA2
1995 Sep 24.00
> million years
Box+ 2 panels
3410 full
1578 empty
2.2x2.5x4
24.5 span
1995
1995
1995
1995
1995
1995
1995
1995
1995
2010
24.24
26.05
27.16
27.26
27.76
1.22
2.33
3.10
3.86
24.17
6.94
4.27
2.32
0.19
0.16
0.23
0.20
0.20
0.21
6.66
Ariane-4 3rd stage
(H-10-3)
+ VEB
1995-49 B
[23671]
1995 Sep 24.00
Cylinder
1250
Cylinder
530
10.2 long
2.6 dia
1 high
4 dia
1995 Sep 24.23
2010 Dec 25.25
7.03
7.00
$
%
&
*
Sep
Sep
Sep
Sep
Sep
Oct
Oct
Oct
Oct
Dec
7.77
8.69
10.81
11.38
14.43
14.73
15.62
17.92
Apogee
height
(km)
1995-48 A
[23667]
CC-LC39
1289
Sep
Sep
Sep
Sep
Sep
Sep
Sep
Sep
Perigee
height
(km)
D STS-069 $
5M Endeavour F9
R [Shuttle]
Nodal
period
(min)
631.88
720.38
866.62
1434.98
1427.68
1435.57
1435.37
1436.12
1436.08
1435.78
24392
26620
30110
41750
42000
42154
42170
42165
42164
42159
655.72 25002
641.33 24635
Astronomy and micro-gravity mission with crew of 5 astronauts (Walker, Cockrell, Voss, Newman and Gernhardt).
Deployed from cargobay by shuttle-arm and releases 1995 Sep 8.65; recaptured 1995 Sep 10.63
Deployed from cargobay by shuttle-arm and releases 1995 Sep 11.48; recaptured 1995 Sep 15.58
Replacement for Telstar 402, launched 1994 Sep 9, which apparently disintegrated shortly after orbital injection.
RAE Table of Earth Satellites (extended)
(Compiled 2006)
Page 1995-22
Launchdate
Lifetime + Descent date
[Norad]
Shape and
weight (kg)
Descent date
Semi
major axis
(km)
Year of Launch 1995
Name
[Launcher]
Fragments
Cospar ID
[Norad #] Launchsite
Cospar ID
Size
(m)
Lifetime
Date of
orbital
determination
Orbital
Inclination
(deg)
Sep
Sep
Sep
Oct
Oct
Oct
Nodal
period
(min)
Perigee
height
(km)
Apogee
height
(km)
Orbital
Argument
eccentricity of perigee
(deg)
D
R
Resurs-F 20
[Soyuz-U]
1995-50 A
[23672]
PLE
1995 Sep 26.47
29.76 days
1995 Oct 26.23
Cyl+ 2 panels+ 6.5 long
sphere+ double 2.4 maxdia
cone
6300
1995
1995
1995
1995
1995
1995
26.90
27.14
27.45
21.79
22.10
26.16
82.32
82.25
82.33
82.32
82.32
82.32
88.77
89.12
89.13
89.02
89.85
89.82
6592
6610
6610
6605
6645
6644
180
184
230
219
255
254
247
278
233
233
278
277
0.005
0.007
0.0003
0.001
0.002
0.002
94
60
87
85
97
81
D
Soyuz-U 3rd stage
(Block I)
1995-50 B
[23673]
1995 Sep 26.47
3 days
1995 Sep 29
Cylinder
2400
8.1 long
2.66 dia
1995 Sep 26.90
1995 Sep 29.04
82.36
82.32
88.83 6586
87.27 6518
179
130
235
149
0.004
0.001
94
62
D
Manoeuvring motor
1995-50 C
[23699]
1995 Sep 26.47
37 days
1995 Nov 2
Cylinder
600
1.9 long
1 dia
1995 Oct 26.47
1995 Nov 2.04
82.32
82.30
89.80 6643
87.35 6521
254
142
276
144
0.002
0.0001
87
288
D
Retrorocket casing 1995-50 E
[23701]
1995 Sep 26.47
42 days
1995 Nov 7
Half hollow
cone
1995 Oct 26.43
1995 Nov 7.54
82.31
82.30
92.17 6759
88.52 6579
270
178
492
224
0.016
0.003
337
273
D
Retrorocket casing 1995-50 F
[23702]
1995 Sep 26.47
45 days
1995 Nov 10
Half hollow
cone
1995 Oct 26.86
1995 Nov 10.30
82.31
82.29
91.67 6735
88.32 6570
270
174
442
209
0.013
0.003
334
279
D
Fragment
1995-50 D
[23700]
1995 Oct 30
34 days
1995 Oct 26.34
1995 Oct 30.68
82.31
82.28
89.78 6642
87.67 6537
253
156
274
161
0.002
0.0003
74
107
D
Cosmos 2320
[Soyuz-U]
1995-51 A
[23674]
BAI
1995 Sep 29.18
365.3 days
1996 Sep 28.5
Cylindrical
7000
7 long
2.5 dia
1995
1995
1995
1995
1995
1995
1995
1995
1995
1995
1996
1996
1996
1996
1996
1996
1996
29.24
29.86
30.17
27.48
27.73
15.84
16.22
25.14
11.48
11.79
18.24
20.24
17.68
18.58
6.29
7.16
28.49
64.92
64.93
64.92
64.92
64.91
64.91
64.91
64.91
64.91
64.91
64.90
64.91
64.90
64.90
64.90
64.90
64.89
89.15
89.75
89.93
89.55
89.77
89.52
89.73
89.85
89.67
90.80
90.18
90.28
89.78
89.92
89.48
89.93
89.32
6611
6641
6650
6630
6642
6629
6639
6646
6637
6692
6662
6667
6642
6649
6628
6650
6619
180
213
240
227
238
229
239
237
232
240
232
243
227
241
228
242
223
284
311
302
277
288
272
283
297
285
387
335
334
300
300
270
300
258
0.008
0.007
0.005
0.004
0.004
0.003
0.003
0.004
0.004
0.011
0.008
0.007
0.006
0.004
0.003
0.004
0.003
71
53
84
62
89
78
106
89
79
118
82
112
62
104
74
108
72
Soyuz-U 3rd stage
(Block I)
1995-51 B
[23675]
1995 Sep 29.18
Cylinder
2400
8.1 long
2.66 dia
1995 Sep 29.43
1995 Oct 2.94
64.92
64.92
88.98 6603
87.32 6520
179
133
269
149
0.007
0.001
69
76
Sep
Sep
Sep
Oct
Oct
Nov
Nov
Nov
Dec
Dec
Mar
Mar
Jun
Jun
Aug
Aug
Sep
RAE Table of Earth Satellites (extended)
(Compiled 2006)
Page 1995-23
Launchdate
Lifetime + Descent date
[Norad]
Shape and
weight (kg)
Descent date
Size
(m)
Lifetime
Date of
orbital
determination
Orbital
Inclination
(deg)
Semi
major axis
(km)
Year of Launch 1995
Name
[Launcher]
Fragments
Cospar ID
[Norad #] Launchsite
Cospar ID
Nodal
period
(min)
Perigee
height
(km)
Apogee
height
(km)
Orbital
Argument
eccentricity of perigee
(deg)
D
Cosmos 2321
[Kosmos-3M]
1995-52 A
[23676]
PLE
1995 Oct 6.14
685 days
1997 Aug 21
Cylinder +
gravity boom
825
2.1 long
2 dia
1995 Oct 6.60
1996 Dec 31.11
1997 Aug 21.53
82.94
82.93
82.89
95.13 6903
92.63 6782
87.15 6507
257
248
127
792
559
130
0.039
0.023
0.0002
84
260
131
D
Kosmos-3M 2nd stage 1995-52 B
[23677]
1995 Oct 6.14
496 days
1997 Mar 13
Cylinder
1434
4.21 long
2.4 dia
1995 Oct 6.53
1997 Mar 13.08
82.94
82.88
95.03 6898
86.92 6500
248
106
791
138
0.039
0.002
85
225
D
Progress-M 29 *
[Soyuz-U]
1995-53 A
[23678]
BAI
1995 Oct 8.79
71.85 days
1995 Dec 19.64
Cyl+ 2 panels+ 7.9 long
1995 Oct 9.09
beehive+sphere 2.72 maxdia 1995 Oct 10.15
7250
1995 Oct 11.03
1995 Dec 18.86
1995 Dec 19.63
51.65
51.65
51.65
51.64
51.64
90.07
90.18
92.43
92.45
92.47
6656
6662
6773
6773
6774
257
260
392
390
391
298
307
396
399
399
0.003
0.004
0.0004
0.0007
0.0006
142
132
169
114
106
D
Soyuz-U 3rd stage
(Block I)
1995-53 B
[23679]
1995 Oct 8.79
2 days
1995 Oct 10
Cylinder
2400
8.1 long
2.66 dia
1995 Oct 9.08
1995 Oct 10.49
51.68
51.67
88.47 6577
87.65 6537
185
153
213
164
0.002
0.0008
85
94
Luch-1 1
[Proton-K]
1995-54 A
[23680]
BAI
1995 Oct 11.68
> million years
Cylindrical
+ 2 panels
2400
5 long
2 dia
1995
1995
1995
2010
11.47
26.77
7.77
26.68
3.03
3.07
3.03
10.25
35864
35766
35758
35754
35962
35809
35812
35815
0.001
0.0005
0.0006
0.0007
235
339
352
326
D
Proton-K 3rd stage
1995-54 B
[23681]
1995 Oct 11.68
3 day
1995 Oct 14
Cylinder
4185
4.0 long
4.1 dia
1995 Oct 11.74
1995 Oct 14.24
51.64
51.64
88.32 6570
87.12 6511
185
129
197
135
0.0009
0.0004
268
28
D
Proton-K 4th stage
casing
1995-54 C
[23682]
1995 Oct 11.68
1 day
1995 Oct 12
Hollow cyl
800
4 long
3.7 dia
1995 Oct 12.17
1995 Oct 12.41
51.64
51.62
88.05 6556
87.07 6508
174
112
182
146
0.0006
0.003
89
196
Proton-K 4th stage
(Block DM-2)
1995-54 D
[23683]
1995 Oct 11.68
> million years
Cylinder
2350
6.22 long
3.7 dia
1995 Oct 12.38
2010 Dec 25.67
3.11
10.23
1436.62 42175
1437.68 42196
35720
35730
35873
35904
0.002
0.002
357
301
D
Ullage motor
1995-54 E
[23684]
1995 Oct 11.68
222 days
1996 May 20
Cylinder
55
0.90 long
0.68 dia
1995 Oct 13.06
1996 May 20.17
47.49
46.72
634.78 24467
93.75 6836
275
88
35902
827
0.728
0.054
0
86
D
Ullage motor
1995-54 F
[23685]
1995 Oct 11.68
296 days
1996 Aug 2
Cylinder
55
0.90 long
0.68 dia
1995 Oct 16.59
1996 Aug 2.14
47.57
46.70
635.85 24494
89.08 6608
325
95
35906
364
0.726
0.020
1
120
*
Progress-M 29 docked 1995 Oct 10.856 with MIR (Kvant port); undocked 1995 Dec 19.385
Oct
Oct
Nov
Dec
1442.58
1436.17
1436.05
1436.00
42292
42166
42164
42163
RAE Table of Earth Satellites (extended)
(Compiled 2006)
Page 1995-24
Launchdate
Lifetime + Descent date
[Norad]
Shape and
weight (kg)
Descent date
Size
(m)
Lifetime
Semi
major axis
(km)
Year of Launch 1995
Name
[Launcher]
Fragments
Cospar ID
[Norad #] Launchsite
Cospar ID
Orbital
Inclination
(deg)
Nodal
period
(min)
Orbital
Argument
eccentricity of perigee
(deg)
502
10282
25659
33680
35705
35703
35768
35845
35834
35737
36070
35878
35872
35805
0.720
0.434
0.136
0.029
0.002
0.002
0.0004
180
180
178
175
225
239
194
1995 Oct 19.03
> million years
Box+2 panels
3010
3.4x2.8
1995 Oct 19.26
4.5-7.8high 1995 Oct 20.73
26.2 span
1995 Oct 22.25
1995 Oct 23.93
1995 Nov 2.99
1995 Nov 18.20
2010 Dec 25.00
4.17
1.56
0.34
0.15
0.10
0.11
0.58
Ariane-4 3rd stage
(H-10-3)
+ VEB
1995-55 B
[23687]
1995 Oct 19.03
Cylinder
1250
Cylinder
530
10.2 long
2.6 dia
1 high
4 dia
1995 Oct 19.26
2010 Dec 25.20
4.22
4.86
653.95 24957
650.70 24874
491
453
36666
36538
0.725
0.725
181
31
1995-56 A
[23688]
CC-LC39
1995 Oct 20.58
16.91 days
1995 Nov 5.49
Delta wing
104399
37.3 long
5.5 dia
23.8 span
1995 Oct 20.70
1995 Nov 4.92
39.01
39.01
89.97 6651
89.73 6640
267
255
278
267
0.0008
0.0008
275
6
UFO 6 (USA 114)
[Atlas-2]
1995-57 A
[23696]
CC
1995 Oct 22.33
> million years
Box+ 2 panels
+ antennae
3000
2.7x2.2x2.6
3.6 to
6.8 high
26.5 span
1995
1995
1995
1995
1995
1995
1995
1997
22.32
24.06
27.49
28.37
29.30
6.24
24.70
31.34
27.00
26.99
7.31
5.30
5.28
5.10
5.00
4.20
276
320
23391
34032
34761
34984
35776
35776
27572
31502
36620
36583
36582
36585
35796
35796
0.672
0.699
0.182
0.031
0.022
0.019
0.0002
0.0002
174
177
180
180
181
179
224
300
Atlas-2 2nd stage
(Centaur)
1995-57 B
[23697]
1995 Oct 22.33
Cylinder
1815
10.1 long
3.05 dia
1995 Oct 22.53
2010 Dec 21.78
26.95
26.87
264
258
27483
19383
0.672
0.590
175
241
479.83
551.97
1151.12
1411.72
1430.27
1436.00
1436.10
1436.05
24553
29437
37076
41254
42170
42166
42165
Apogee
height
(km)
1995-55 A
[23686]
KOU-ELA2
Oct
Oct
Oct
Oct
Oct
Nov
Dec
Dec
638.12
837.70
1184.13
1389.80
1436.37
1436.17
1436.12
Perigee
height
(km)
Astra 1E
[Ariane-42L]
(#49)
D STS-073 $
7M Columbia F18
R [Shuttle]
$
Date of
orbital
determination
20303
22290
36384
41686
42051
42163
42165
42165
478.08 20254
341.98 16199
US Microgravity Laboratory-2 mission with 7 astronauts (Bowersox, Rominger, Thornton, Coleman, Lopez-Alegria, Leslie and Sacco)
Year of Launch 1995
Name
[Launcher]
Fragments
D
D
Cospar ID
[Norad #] Launchsite
Cospar ID
RAE Table of Earth Satellites (extended)
(Compiled 2006)
Page 1995-25
Shape and
weight (kg)
Descent date
Semi
major axis
(km)
Size
(m)
Lifetime
Date of
orbital
determination
Orbital
Inclination
(deg)
1995 Oct 31.98
2010 Dec 26.95
70.02
70.98
1995 Nov 1.19
2010 Dec 25.44
Nodal
period
(min)
Perigee
height
(km)
Apogee
height
(km)
Orbital
Argument
eccentricity of perigee
(deg)
101.93 7229
101.88 7227
849
843
852
853
0.0002
0.0007
69
73
71.04
71.02
101.83 7224
101.77 7221
842
832
848
853
0.0004
0.001
70
298
Cosmos 2322
[Zenit-2]
1995-58 A
[23704]
BAI
1995 Oct 31.85
Zenit-2 2nd stage
1995-58 B
[23705]
1995 Oct 31.85
Separation
Motor cap
1995-58 C
[23706]
1995 Oct 31.85
1995 Nov 1.21
2010 Dec 25.48
71.01
71.00
104.97 7372
104.87 7367
845
840
1142
1136
0.020
0.020
70
149
Separation
Motor cap
1995-58 D
[23707]
1995 Oct 31.85
1995 Nov 1.50
2010 Dec 26.52
71.00
71.00
105.08 7377
105.00 7373
847
842
1150
1146
0.021
0.021
92
195
Separation
Motor cap
1995-58 E
[23708]
1995 Oct 31.85
1995 Nov 1.50
2010 Dec 25.45
71.05
71.05
104.78 7362
104.68 7358
846
844
1122
1115
0.019
0.018
72
76
Separation
Motor cap
1995-58 F
[23709]
1995 Oct 31.85
1995 Nov 1.50
2010 Dec 25.56
71.05
71.04
104.95 7370
104.83 7365
845
840
1139
1133
0.020
0.020
98
137
Fragments
1995-58 G-K
4 pieces, all have decayed
For orbital information see extra pages at end of year
Radarsat 1
[Delta-2]
1995-59 A
[23710]
VDB
1995 Nov 4.60
Box+ 2 panels
+ radarpanel
1995 Nov 4.85
1995 Dec 16.53
2010 Dec 28.92
98.59
98.58
98.58
100.57 7164
100.70 7170
100.70 7170
783
791
791
787
792
792
0.0003
0.00009
0.0001
81
90
91
Delta-2 2nd stage
+ SURFsat *
1995-59 B
[23711]
1995 Nov 4.60
Cylinder
919 + 41
5.88 long
2.44 dia
1995 Nov 4.87
2010 Dec 28.52
100.64
100.33
109.73 7593
109.70 7591
934
933
1494
1492
0.037
0.037
238
283
Fragment #
1995-59 C
[23749]
2002 Apr 1
2007 Apr 27
2340 days
4192 days
1996
2002
2007
2007
100.64
100.79
99.36
99.47
109.70
92.62
106.78
93.72
932
369
442
280
1493
436
1712
632
0.037
0.005
0.085
0.026
28
291
145
140
1995-59 D
*
#
Launchdate
Lifetime + Descent date
[Norad]
3250
[31143]
Cylinder
8300
10.41 long
3.9 dia
Feb
Mar
Apr
Apr
5.96
31.68
17.59
27.26
Summer Undergraduate Research Fellowship Satellite remained attached to Delta-2 2nd stage.
One piece was liberated. Event was 1996 Jan 30.
7591
6781
7456
6835
RAE Table of Earth Satellites (extended)
(Compiled 2006)
Page 1995-26
Launchdate
Lifetime + Descent date
[Norad]
Shape and
weight (kg)
Descent date
Size
(m)
Lifetime
Date of
orbital
determination
Semi
major axis
(km)
Year of Launch 1995
Name
[Launcher]
Fragments
Cospar ID
[Norad #] Launchsite
Cospar ID
Orbital
Inclination
(deg)
Nodal
period
(min)
Perigee
height
(km)
Apogee
height
(km)
Orbital
Argument
eccentricity of perigee
(deg)
6697
6748
6772
6771
6770
6721
6720
299
346
390
391
388
336
336
339
394
395
394
395
348
346
0.003
0.004
0.0004
0.0002
0.0005
0.0009
0.0008
357
303
335
344
332
267
277
42405
42185
42187
41717
574
1036
1117
655
71478
70578
70501
70021
0.836
0.824
0.822
0.831
114
116
116
121
Milstar DFS 2
[Titan-4}
1995-60 A
[23712]
CC
1995 Nov 6.22
> million years
Boxes
4670
47 long
106 span
No TLE available
Titan-4 3rd stage
(Centaur)
1995-60 B
[23713]
1995 Nov 6.22
Cylinder
2700
9.0 long
4.3 dia
No TLE available
D STS-074 *
5M Atlantis F15
R [Shuttle]
1995-61 A
[23714]
CC-LC39
1995 Nov 12.52
8.19 days
1995 Nov 20.71
Delta wing
93000
37.3 long
5.5 dia
23.8 span
1995
1995
1995
1995
1995
1995
1995
Nov
Nov
Nov
Nov
Nov
Nov
Nov
12.85
13.68
15.27
17.92
18.42
18.67
20.25
51.64
51.64
51.65
51.64
51.64
51.64
51.64
ISO
[Ariane-44P]
(#50)
1995-62 A
[23715]
KOU-ELA2
1995 Nov 17.06
Cylindrical
3.56x2.77
x5.31 high
1995
1995
1995
2010
Nov
Nov
Dec
Dec
17.02
27.71
2.10
28.05
5.20
5.18
5.10
3.53
1448.37
1437.15
1437.25
1413.27
Ariane-4 3rd stage
(H-10-3)
+ VEB
1995-62 B
[23716]
1995 Nov 17.06
Cylinder
1250
Cylinder
530
10.2 long
2.6 dia
1 high
4 dia
1995 Nov 17.03
2010 Dec 28.83
5.19
2.22
1475.05 42924
1515.92 43713
537
929
72554
73740
0.839
0.833
113
118
Fragment
1995-62 C
[24700]
1996 Dec 15.64
2003 Sep 12.21
2010 Dec 18.87
1.37
3.02
2.90
1435.13 42146
1435.15 42146
1434.82 42140
1080
1118
1167
70454
70417
70355
0.823
0.822
0.820
177
112
120
GALS 2
[Proton-K]
1995-63 A
[23717]
BAI
1995 Nov 17.60
> million years
Cylinder +
2 booms with
solarpanels
2500
6.6 long
2.1 dia
1995
1995
1995
1995
1995
1995
2010
0.20
0.20
0.15
0.15
0.15
0.17
9.24
1442.35
1436.00
1436.08
1436.30
1436.15
1436.10
1441.63
35788
35751
35762
35781
35777
35784
35862
36029
35818
35810
35799
35798
35788
35927
0.003
0.0008
0.0006
0.0002
0.0002
0.00005
0.0008
82
328
342
49
91
118
204
Proton-K 3rd stage
1995-63 B
[23718]
1995 Nov 17.60
4 day
1995 Nov 21
Cylinder
4185
4.0 long
4.1 dia
1995 Nov 17.84
1995 Nov 21.03
187
122
198
124
0.0008
0.0002
337
15
D
Nov
Dec
Dec
Dec
Dec
Dec
Dec
18.31
4.60
4.71
13.77
21.78
28.30
27.06
51.62
51.61
90.90
91.95
92.42
92.40
92.38
91.38
91.35
42287
42163
42165
42169
42166
42165
42273
88.35 6571
86.95 6501
1995 63 continued on next page.
*
Shuttle-MIR-Mission 2 with crew of 5 astronauts (Cameron, Halsell, Hadfield, Ross and McArthur) docked with MIR (Kristall module) 1995 15.27; undocking
1995 Nov 18.34. Shuttle carried Docking-adaptor 316 GK (4.7 long, 2.2 dia, 4087 kg) that remained attached to Kristall.
RAE Table of Earth Satellites (extended)
(Compiled 2006)
Page 1995-27
Launchdate
Lifetime + Descent date
[Norad]
Shape and
weight (kg)
Descent date
Size
(m)
Lifetime
Date of
orbital
determination
Orbital
Inclination
(deg)
Semi
major axis
(km)
Year of Launch 1995
Name
[Launcher]
Fragments
Cospar ID
[Norad #] Launchsite
Cospar ID
Nodal
period
(min)
Perigee
height
(km)
Apogee
height
(km)
Orbital
Argument
eccentricity of perigee
(deg)
175
166
184
174
0.0007
0.0006
70
88
35696
35589
35009
35958
0.004
0.004
47
29
D
Proton-K 4th stage
casing
1995-63 C
[23719]
1995 Nov 17.60
1 day
1995 Nov 18
Hollow cyl
800
4 long
3.7 dia
1995 Nov 18.14
1995 Nov 18.27
51.61
51.61
88.08 6558
87.90 6549
D
Proton-K 4th stage
(Block DM-2)
1995-63 D
[23720]
1995 Nov 17.60
> million years
Cylinder
2350
6.22 long
3.7 dia
1995 Nov 18.59
2010 Dec 28.50
0.24
11.83
1439.48 42231
1435.43 42152
D
Ullage motor
1995-63 E
[23721]
1995 Nov 17.60
209 days
1996 Jun 13
Cylinder
55
0.90 long
0.68 dia
1995 Nov 20.30
1993 Jun 13.29
47.46
46.68
634.27 24454
126.05 8328
255
98
35896
3800
0.729
0.222
1
74
D
Ullage motor
1995-63 F
[23722]
1995 Nov 17.60
772 days
1997 Dec 18
Cylinder
55
0.90 long
0.68 dia
1995 Nov 23.83
1994 Dec 13.66
47.47
46.49
634.98 24472
99.48 7113
313
116
35874
1351
0.727
0.087
2
125
Amos 5I
(ex AsiaSat 2)
[CZ-2E]
1995-64 A
[23723]
XI
1995 Nov 28.48
> million years
Box+ 2 panels
3379
2.16x2.46
x3.15
23 span
1995
1995
1995
1995
1995
1996
2010
29.19
30.06
4.93
5.35
9.77
18.63
27.59
25.59
14.04
0.58
0.45
0.43
0.19
0.33
220
5265
34375
34556
35778
35779
35775
35037
35257
35932
36514
35853
35794
35799
0.725
0.555
0.019
0.023
0.0009
0.0002
0.0003
180
175
281
271
206
68
203
CZ-2E 2nd stage
1995-64 B
[23724]
1995 Nov 28.48
7 days
1995 Dec 5
Cylinder
5500
15.52 long
3.35 dia
1995 Nov 28.84
1995 Dec 5.11
28.01
28.00
89.30 6619
87.60 6534
187
146
293
165
0.008
0.001
138
248
CZ-2E 3rd stage
SPTM-17 PKM
1995-64 C
[23725]
1995 Nov 28.48
Cone-spheroid
535
3.07 long
1.7 maxdia
1995 Nov 29.20
2010 Dec 27.87
25.58
25.68
616.90 24005
631.55 15868
214
269
35040
18711
0.725
0.581
180
53
Fragment
1995-64 D
[28062]
2970 days
2884 days
2003 Oct 27.98
2004 Jan 10.43
2003 Oct 18.04
25.40
25.32
25.43
244.40 12949
109.45 7580
140.98 8974
173
160
175
12968
2243
5014
0.494
0.137
0.270
121
76
211
D
D
Nov
Nov
Dec
Dec
Dec
Jan
Dec
616.97
760.98
1403.88
1423.28
1437.58
1436.10
1436.12
24007
26140
42532
41914
42194
42165
42165
1995-64 E
[28063]
2004 Jan 15
2003 Nov 21
1995-65 A
[23726]
CC
1995 Dec 2.34
Indefinite
Cyl+ 2 panels
1875
3.6 long
3 dia
At L1 libaration point, 1.5 million km from Earth on the Earth-Sun line
No orbital data issued
Atlas-2AS 2nd stage 1995-65 B
(Centaur)
[23727]
1995 Dec 2.34
Indefinite
Cylinder
1835
10.1 long
3.05 dia
Solar orbit
No orbital data issued
D
SOHO
[Atlas-2AS]
RAE Table of Earth Satellites (extended)
(Compiled 2006)
Page 1995-28
Launchdate
Lifetime + Descent date
[Norad]
Shape and
weight (kg)
Descent date
Semi
major axis
(km)
Year of Launch 1995
Name
[Launcher]
Fragments
D
Cospar ID
[Norad #] Launchsite
Cospar ID
Date of
orbital
determination
Orbital
Inclination
(deg)
97.89
97.93
Nodal
period
(min)
Apogee
height
(km)
Orbital
Argument
eccentricity of perigee
(deg)
403
404
838
834
0.031
0.031
319 #
194 #
1995-66 A
[23728]
VDB
1995 Dec 5.89
Cylindrical
19.5 long
+ solar panels 3 dia
13500
2007 Jul 28.05
2008 Nov 18.70
Titan-4 2nd stage
1995-66 B
[23729]
1995 Dec 5.89
Cylinder
2000
9.94 long
3.05 dia
No TLE issued.
Telecom 2C
[Ariane-44L]
(#51)
1995-67 A
[23730]
KOU-ELA2
1995 Dec 6.97
> million years
Box+2 panels
2283 full
1120 empty
1.90x2.60
x3.10
22 span
1995
1995
1996
2010
Dec
Dec
Dec
Dec
7.21
21.75
13.24
26.90
6.99
0.14
0.04
6.52
630.10
1435.90
1436.08
1470.25
24347
42161
42165
42831
224
35765
35765
36377
35712
35800
35807
36527
0.729
0.0004
0.0005
0.002
178
265
94
163
INSAT 2C
1995-67 B
[23731]
1995 Dec 6.97
> million years
Box+ 2 panels
2050 full
980 empty
2.3x2.5x2.7 1995 Dec
14.6 span
1995 Dec
1995 Dec
1995 Dec
2010 Dec
7.21
17.52
19.37
21.26
27.16
6.99
0.30
0.16
0.16
8.01
630.23
1437.73
1435.17
1436.10
1443.22
24350
41805
42147
42165
42304
224
35036
35718
35755
35896
35719
35817
35818
35817
35955
0.729
0.009
0.001
0.0007
0.0007
178
199
220
247
233
Ariane-4 3rd stage
(H-10-3)
+ VEB
1995-67 C
[23732]
1995 Dec 6.97
Cylinder
1250
Cylinder
530
10.2 long
2.6 dia
1 high
4 dia
1995 Dec 7.22
2010 Dec 27.07
6.82
6.86
659.68 25103
535.10 21833
273
306
37175
30603
0.735
0.694
178
73
Mini-Spelda
Upper section
1995-67 D
[23733]
1995 Dec 6.97
2230 days
2002 Jan 13
Hollow cyl
300
1.8 long
4 dia
1995 Dec 7.21
2002 Jan 13.34
6.98
7.18
631.10 24385
88.92 6600
227
126
35786
316
0.729
0.014
178
17
Cosmos 2323
(Glonass 77)
[Proton-K]
1995-68 A
[23734]
BAI
1995 Dec 14.26
1 million years
Cyl +2 panels
1300
1995
1995
1995
1995
1996
2010
14.27
17.08
21.77
23.63
9.31
27.26
64.82
64.83
64.85
64.83
64.83
66.45
675.07
675.63
729.98
726.83
675.75
675.72
25491
25506
25363
25284
25509
25508
19095
19113
18825
18678
19085
19084
19131
19142
19144
19132
19175
19175
0.0007
0.0006
0.006
0.009
0.002
0.002
255
211
240
252
329
278
Cosmos 2324
(Glonass 78)
1995-68 B
[23735]
1995 Dec 14.26
1 million years
Cyl +2 panels
1300
1995 Dec 14.42
1995 Dec 17.64
2010 Dec 28.31
64.78
64.83
66.45
677.60 25555
675.68 25507
675.72 25508
19177
19116
19110
19177
19141
19149
0
0.0005
0.0008
186
214
213
Cosmos 2358
(Glonass 79)
1995-68 C
[23736]
1995 Dec 14.26
1 million years
Cyl +2 panels
1300
1995
1995
1995
1995
1996
2010
64.78
64.83
65.08
64.84
64.82
66.45
677.60
675.68
675.87
675.75
675.72
675.73
19177
19109
19117
19114
19113
19111
19177
19148
19148
19146
19146
19148
0
0.0008
0.0006
0.0006
0.0007
0.0007
186
209
177
190
186
203
TLE from amateur observations
Dec
Dec
Dec
Dec
Jan
Dec
Dec
Dec
Dec
Dec
Jan
Dec
14.42
17.08
24.12
25.06
3.45
27.02
97.12 6999
97.08 6998
Perigee
height
(km)
USA 116
[Titan-4]
1995 68 continued on next page.
#
Size
(m)
Lifetime
25555
25507
25512
25509
25508
25508
RAE Table of Earth Satellites (extended)
(Compiled 2006)
Page 1995-29
Launchdate
Lifetime + Descent date
[Norad]
Shape and
weight (kg)
Descent date
Size
(m)
Lifetime
Date of
orbital
determination
Orbital
Inclination
(deg)
Semi
major axis
(km)
Year of Launch 1995
Name
[Launcher]
Fragments
Cospar ID
[Norad #] Launchsite
Cospar ID
Nodal
period
(min)
Perigee
height
(km)
Apogee
height
(km)
Orbital
Argument
eccentricity of perigee
(deg)
D
Proton-K 3rd stage
1995-68 D
[23737]
1995 Dec 14.26
<1 day
1995 Dec 15
Cylinder
4185
4 long
4.1 dia
1995 Dec 14.56
1995 Dec 14.94
64.82
64.82
87.60 6534
87.20 6514
151
131
160
140
0.0007
0.0007
244
257
D
Proton-K 4th stage
Casing
1995-68 E
[23738]
1995 Dec 14.26
< 0.4 day
1995 Dec 14.6
Hollow cyl
800
4.0 long
3.7 dia
1995 Dec 12.50
1995 Dec 14.56
64.85
64.80
87.62 6535
86.85 6497
138
112
174
124
0.003
0.0009
51
357
Proton-K 4th stage
(Block DM-2)
1995-68 F
[23739]
1995 Dec 14.26
1 million years
Cylinder
2350
6.22 long
3.7 maxdia
1995 Dec 14.74
2010 Dec 27.50
64.81
66.45
675.63 25506
674.87 25486
19093
19085
19161
19130
0.001
0.0009
225
215
D
Ullage motor
1995-68 G
[23740]
1995 Dec 14.26
2171 days
2001 Nov 23
Cylinder
55
0.90 long
0.68 dia
1995 Dec 14.55
2001 Nov 22.66
64.85
63.96
340.20 16143
91.98 6750
388
96
19141
647
0.581
0.041
298
209
D
Ullage motor
1995-68 H
[23743]
1995 Dec 14.26
2130 days
2001 Oct 13
Cylinder
55
0.90 long
0.68 dia
1995 Dec 17.66
2001 Oct 12.68
64.85
63.92
340.12 16140
89.12 6610
388
89
19136
373
0.581
0.022
297
212
Galaxy 3R
[Atlas-2A]
1995-69 A
[23741]
CC
1995 Dec 15.02
> million years
?? + 2 panels
2980
24.7 span
1995
1995
1995
1995
1996
1996
2010
15.14
16.54
23.33
26.81
17.29
26.16
29.14
26.94
26.91
1.43
0.06
0.06
0.05
5.81
200
199
29768
35755
35763
35777
35763
34348
35778
35807
35792
35812
35796
35790
0.722
0.730
0.077
0.0004
0.0006
0.0002
0.00032
178
178
179
302
39
58
255
Atlas-2A 2nd stage
(Centaur 120)
1995-69 B
[23742]
1995 Dec 15.02
Cylinder
1815
10.1 long
3.05 dia
1995 Dec 15.24
2002 Mar 16.02
26.94
26.56
196
116
34240
323
0.721
0.016
178
66
D
Progress-M 30 *
[Soyuz-U]
1995-70 A
[23744]
BAI
1995 Dec 18.60
66.00 days
1996 Feb 22.60
Cyl+ 2 panels+ 7.9 long
1995 Dec 18.84
beehive+sphere 2.72 maxdia 1995 Dec 19.84
7250
1995 Dec 20.91
1995 Feb 21.85
51.64
51.64
51.65
51.65
89.90
90.12
92.45
92.45
6648
6659
6773
6773
240
247
390
390
298
314
399
398
0.004
0.005
0.0006
0.0006
144
127
122
20
D
Soyuz-U 3rd stage
(Block I)
1995-70 B
[23745]
1995 Dec 18.60
3 days
1995 Dec 21
Cylinder
2400
51.64
51.64
88.48 6578
87.25 6517
191
136
207
139
0.001
0.0002
73
342
*
Progress-M 30 docked 1995 Dec 20.674 with MIR (Kvant port); undocked 1996 Feb 22.310
8.1 long
2.66 dia
Dec
Dec
Dec
Dec
Jan
Jan
Dec
1995 Dec 18.78
1995 Dec 21.23
603.37
630.90
1285.65
1435.45
1436.17
1436.10
1435.58
23653
24367
39166
42152
42166
42165
42155
601.22 23597
88.88 6598
RAE Table of Earth Satellites (extended)
(Compiled 2006)
Page 1995-30
Launchdate
Lifetime + Descent date
[Norad]
Shape and
weight (kg)
Descent date
Size
(m)
Lifetime
Date of
orbital
determination
Orbital
Inclination
(deg)
Semi
major axis
(km)
Year of Launch 1995
Name
[Launcher]
Fragments
Cospar ID
[Norad #] Launchsite
Cospar ID
Nodal
period
(min)
Perigee
height
(km)
Apogee
height
(km)
Orbital
Argument
eccentricity of perigee
(deg)
D
Cosmos 2326
(US-P)
[Tsyklon-M]
1995-71 A
[23748]
BAI
1995 Dec 20.04
689 days
1997 Nov 8
Cylindrical +
stubby cyl
+ 2 panels
3150
6 long
2 dia
1.5 long
3 dia
1995 Dec 20.16
1997 Nov 8.06
65.02
64.97
92.77 6789
87.23 6516
406
127
414
147
0.0006
0.002
235
282
D
Tsyklon-M 2nd stage 1995-71 B
[23750]
1995 Dec 20.04
<0.5 day
1995 Dec 20.5
Cylinder
4000
10.9 long
3 dia
1995 Dec 20.09
1995 Dec 20.40
64.99
65.00
89.50 6628
88.30 6569
112
106
387
275
0.021
0.013
53
56
D
Fragments
[24456]
1998 Oct 9
1024 days
1998 Dec 11
1087 days
1996
1998
1997
1998
3.06
9.14
29.27
11.09
65.02
64.99
65.01
64.99
92.78
87.93
92.80
87.97
6790
6550
6790
6553
403
165
406
171
420
178
417
177
0.001
0.001
0.0008
0.0005
300
259
278
255
D
D
1995-71 C
1995-71 D
[24816]
Oct
Oct
May
Dec
IRS-1C
[Molniya-M]
1995-72 A
[23751]
BAI
1995 Dec 28.28
Box+ 2 panels
1350
1.6x1.56
x1.1
1995 Dec 28.40
2010 Dec 29.08
98.60
98.38
101.12 7190
101.27 7197
805
818
817
819
0.0008
0.0001
156
93
Skipper
1995-72 B
[23752]
1995 Dec 28.28
Cylinder
230
1.3 long
0.8 dia
1995 Dec 29.10
2010 Dec 28.90
98.57
98.62
101.05 7187
101.00 7185
804
803
813
810
0.0007
0.0005
130
296
Molniya-M 4th stage 1995-72 C
(Block 2BL)
[23753]
1995 Dec 28.28
Cylinder
900
2.3 long
2.2 dia
1995 Dec 29.17
2010 Dec 27.46
98.60
98.60
101.03 7187
100.97 7183
805
802
811
807
0.0005
0.0003
122
295
Echostar 1
[CZ-2E]
1995-73 A
[23754]
XI
1995 Dec 28.49
> million years
Box+ 2 panels
3288
2.16x2.46
x3.15
24.3 span
1995
1996
1996
1996
2010
28.79
2.53
22.62
29.66
27.04
24.39
5.05
0.11
0.09
0.03
222
17561
35765
35764
35775
35081
35071
35810
35809
35798
0.725
0.268
0.0005
0.0005
0.0003
179
181
40
41
355
CZ-2E 2nd stage
1995-73 B
[23755]
1995 Dec 28.49
9 days
1996 Jan 6
Cylinder
5500
15.52 long
3.35 dia
1995 Dec 28.73
1996 Jan 5.55
28.00
28.00
89.33 6620
88.12 6559
191
162
291
200
0.008
0.003
130
242
CZ-2E 3rd stage
SPTM-17 PKM
1995-73 C
[23756]
1995 Dec 28.49
Cone-spheroid
535
3.07 long
1.7 maxdia
1995 Dec 29.22
2010 Dec 28.82
24.38
24.15
617.82 24029
473.57 20126
223
252
35078
27242
0.725
0.671
179
310
Dec
Jan
Jan
Jan
Dec
617.85
980.57
1436.15
1436.10
1436.12
24030
32695
42166
42165
42165
RAE Table of Earth Satellites (extended)
(Compiled 2006)
Page 1995-31
Launchdate
Lifetime + Descent date
[Norad]
Shape and
weight (kg)
Descent date
Size
(m)
Lifetime
Semi
major axis
(km)
RXTE *
1995-74 A
[Delta-2(7920-10)] [23757]
CC
1995 Dec 30.58
Box+ 2 panels
3035
1.8x1.8x3.9 1995 Dec 30.62
2010 Dec 29.17
22.98
22.98
D
Delta-2 2nd stage
1995-74 B
[23758]
1995 Dec 30.58
24 days
1996 Jan 23
Cylinder
919
5.88 long
2.44 dia
24.95
24.93
D
Fragments
1995-74 C-E
3 pieces, all have decayed
*
In orbit XTE (X-ray Timing Explorer) was re-named Bruno B Rossi X-ray Timing Explorer (RXTE).
Year of Launch 1995
Name
[Launcher]
Fragments
Cospar ID
[Norad #] Launchsite
Cospar ID
Date of
orbital
determination
1995 Dec 30.75
1996 Jan 23.09
Orbital
Inclination
(deg)
Nodal
period
(min)
Perigee
height
(km)
Apogee
height
(km)
Orbital
Argument
eccentricity of perigee
(deg)
96.15 6953
94.18 6858
565
473
583
485
0.001
0.0008
188
168
92.28 6765
87.55 6532
178
133
596
172
0.031
0.003
264
221
For orbital information see extra pages at end of year
RAE Table of Earth Satellites
Year of Launch 1995
Cospar ID
[Norad number]
Descent date
Lifetime
Date of
orbital
Determination
(Compiled 2006)
Orbital
Inclination
(deg)
Nodal
period
(min)
Extra Page 1995 -1
Semi
major axis
(km)
Perigee
height
(km)
Apogee
height
(km)
Orbital
eccentric.
Argument
of perigee
(deg)
Text in box is from "History of on-orbit satellite fragmentations", 13th edition, May 2004.
Orbital Debris Program Office, Johnson Space Centre, NASA, Houston, TX 77058.
Cosmos 2306 fragments; 13 pieces, all have decayed.
D 1995-08 N
[26584]
2000 Oct 25
D 1995-08 P
[26585]
2000 Oct 28
D 1995-08 Q
[26586]
2000 Oct 27
D 1995-08 R
[26587]
2000 Oct 27
D 1995-08 S
[26588]
2000 Oct 27
D 1995-08 T
[26589]
2000 Oct 27
D 1995-08 U
[26592]
2000 Oct 29
D 1995-08 V
[26593]
2000 Oct 29
D 1995-08 W
[26594]
2000 Oct 29
D 1995-08 X
[26595]
2000 Oct 29
D 1995-08 Y
[26596]
2000 Oct 29
D 1995-08 Z
[26597]
2000 Oct 29
D 1995-08 AA
[26598]
2000 Oct 29
DMSP-2 8 fragments; 4 pieces, all in orbit.
1995-15 B
[23534]
1995-15 C
[23535]
1995-15 D
[23594]
1995-15 E
[23595]
ERS 2 fragments; 6 pieces, 1 have decayed
D 1995-21 C
[28066]
2006 Apr 16
1995-21 D
[31137]
1995-21 E
[35391]
1995-21 F
[35392]
1995-21 G
[35393]
1995-21 H
[39478]
2064 days
2067 days
2066
2066
2066
2066
2068
days
days
days
days
days
2068 days
2068 days
2068 days
2068 days
2068 days
2068 days
2000
2000
2000
2000
2000
2000
2000
2000
2000
2000
2000
2000
2000
2000
2000
2000
2000
2000
2000
2000
Oct
Oct
Oct
Oct
Oct
Oct
Oct
Oct
Oct
Oct
Oct
Oct
Oct
Oct
Oct
Oct
Oct
Oct
Oct
Oct
25.00
25.35
25.23
28.18
27.14
27.33
27.21
27.21
27.14
29.67
29.67
29.68
29.68
29.67
29.67
29.73
29.67
29.68
29.67
29.73
65.81
65.80
65.84
65.82
65.81
65.84
65.81
65.81
65.81
65.81
65.82
65.82
65.80
65.81
65.80
65.84
65.80
65.82
65.82
65.82
88.93
88.52
89.08
87.38
88.47
88.12
88.72
88.23
88.07
87.25
87.17
87.12
87.43
87.65
87.68
87.47
87.70
87.88
87.77
87.27
6600
6580
6607
6524
6578
6560
6590
6566
6557
6516
6513
6510
6525
6537
6538
6528
6540
6548
6542
6517
214
195
216
112
198
178
199
182
172
130
129
125
133
154
154
122
151
148
157
124
230
208
242
177
200
185
223
192
185
145
139
138
160
162
165
176
170
192
170
153
0.001
0.001
0.002
0.005
0.0002
0.0006
0.002
0.0007
0.001
0.001
0.0008
0.001
0.002
0.0005
0.0009
0.004
0.001
0.003
0.001
0.0023
233
269
133
275
221
320
195
290
233
348
233
158
347
240
317
344
334
134
333
324
1995
2005
2010
1995
2005
2010
1995
2005
2010
1995
2005
2010
Mar
Feb
Dec
Mar
Feb
Dec
Apr
Feb
Dec
Apr
Feb
Dec
28.24
19.24
24.07
26.83
19.56
23.28
9.00
20.22
22.60
9.00
18.70
22.50
98.83
98.74
99.02
98.83
98.74
98.61
98.84
98.72
98.78
98.83
98.71
98.75
101.92
99.48
98.79
101.93
100.50
100.23
101.92
99.37
98.83
101.92
99.72
99.28
7228
7113
7090
7228
7161
7148
7228
7107
7061
7228
7123
7103
847
732
711
846
777
764
845
725
702
845
739
721
851
736
712
853
787
775
855
731
704
854
750
728
0.0003
0.0002
0.00008
0.0005
0.0006
0.0008
0.0007
0.0004
0.0001
0.0006
0.0007
0.0005
129
134
180
147
313
133
207
116
140
216
241
302
2003
2006
2007
2009
2009
2009
2014
Oct
Apr
May
Jun
Jun
Jun
Jan
26.26
17.55
8.60
21.13
22.18
21.67
13.56
98.32
98.31
98.38
98.44
98.55
98.40
98.56
96.55
90.03
100.42
100.60
100.47
100.30
95.37
6972
6655
7157
7165
7159
7151
6915
586
263
776
783
777
769
534
601
289
780
791
784
776
538
0.001
0.002
0.0003
0.0006
0.0004
0.0005
0.0003
161
263
137
325
63
320
180
RAE Table of Earth Satellites
Year of Launch 1995
Cospar ID
[Norad number]
Descent date
Lifetime
Date of
orbital
Determination
(Compiled 2006)
Orbital
Inclination
(deg)
Nodal
period
(min)
Extra Page 1995 -2
Semi
major axis
(km)
Perigee
height
(km)
Apogee
height
(km)
Orbital
eccentric.
Argument
of perigee
(deg)
Cosmos 2313 fragments; 12 pieces, all have decayed.
Cosmos 2313 was the second spacecraft of its type to breakup since November 1987. Prior to the current event 17 spacecraft of this class (Cosmos 699) have experienced breakups in low Earth orbit. In the 1980's procedures were
introduced to deplete remaining propellants at the end of mission, reducing orbital lifetime at the same time. Cosmos 2313 performed such a maneuver during 22-23 April 1997 and was close to reentry at the time of the event. Earlier
spacecraft breakups resulted in up to 150 or more trackable debris. The cause of the event may well not be propellant related, but by reducing the orbital lifetime recent vehicles have decayed before the trigger mechanism could activate.
At least 90 debris were detected after this event.
D 1995-28 C
[24853]
1997 Jul 7.77
64.87
92.43 6772
274
513
0.018
130
1997 Jul 30
783 days
1997 Jul 29.88
64.85
88.58 6583
190
218
0.002
153
D 1995-28 D
[24854]
1997 Jul 7.78
64.90
91.83 6743
264
465
0.015
139
1997 Jul 18
771 days
1997 Jul 18.50
64.89
89.00 6603
198
252
0.004
145
D 1995-28 E
[24855]
1997 Jul 7.83
64.88
93.20 6810
275
587
0.023
135
1997 Sep 25
840 days
1997 Sep 25.45
64.87
88.97 6602
190
257
0.005
93
D 1995-28 F
[24856]
1997 Jul 7.45
65.08
93.75 6837
269
648
0.028
139
1997 Jul 25
778 days
1997 Jul 22.54
65.09
90.88 6696
263
372
0.008
129
D 1995-28 G
[24857]
1997 Jul 7.74
64.89
92.97 6798
277
563
0.021
133
1997 Sep 23
838 days
1997 Sep 23.46
64.87
89.05 6606
202
252
0.004
77
D 1995-28 H
[24858]
1997 Jul 7.68
64.92
91.67 6735
271
441
0.013
130
1997 Jul 24
777 days
1997 Jul 24.13
64.91
88.92 6600
206
236
0.002
133
D 1995-28 J
[24859]
1997 Jul 8.17
64.91
91.48 6726
264
431
0.012
142
1997 Jul 16
769 days
1997 Jul 15.70
64.88
88.77 6592
204
222
0.001
123
D 1995-28 K
[24860]
1997 Jul 8
761 days
1997 Jul 7.47
64.98
88.78 6593
207
222
0.001
173
D 1995-28 L
[24861]
1997 Jul 8.09
64.94
91.07 6706
268
386
0.009
142
1997 Jul 29
782 days
1997 Jul 28.48
64.92
88.80 6594
204
226
0.002
137
D 1995-28 M
[24862]
1997 Jul 7
760 days
1997 Jul 6.44
65.01
87.92 6550
154
189
0.003
265
D 1995-28 N
[24863]
1997 Jul 7.42
64.99
90.73 6689
254
366
0.008
144
1997 Jul 12
765 days
1997 Jul 11.80
64.97
88.62 6585
185
227
0.003
156
D 1995-28 P
[24864]
1997 Jul 7.70
64.89
91.13 6709
260
400
0.010
136
1997 Jul 11
764 days
1997 Jul 11.59
64.88
89.08 6608
200
259
0.004
127
Cerise, 1995-33B and Spot 1 debris, 1986-19 RF
The incident marked the first time that two objects in the US satellite catalogue are known to have accidentally run into one another. The CERISE spacecraft (Satellite Number 23606, International Designator 1995-033B) is a microsatellite of
British design. The other participant in the encounter was Satellite Number 18208 (International Designator 1986-019RF) which was generated in November 1986, when ESA's SPOT 1 rocket body broke-up into nearly 500 tracked debris. The
orbit of this fragmentation debris at the time of the collision was 660 km by 680 km at an inclination of 98.45 degrees. The collision, which occurred with a relative velocity of 14.8 km/s, produced only a single piece of debris large enough to
be tracked, i.e., the upper portion of the gravity-gradient boom. Analysis of the manufacturer of the spacecraft bus, Surrey Satellite Technology Ctd. At the University of Surrey, United Kingdom suggested that the 6 m, gravity-gradient boom
had been severed at 3.1-3.2 meter from its base.
Using USAF Space Command's COMBO (Computation of Miss Between Orbits) program, a close approach of less than 1 km between Satellite 23606 and Satellite 18208 was determined by NASA JSC to have taken place at 0948 GMT on 24
July 1996 over the southern Indian Ocean. Naval Space Operations Center (NAVSPOC) at Dahlgren, Virginia, replicated the NASA findings and, using direct observational data and special perturbation theory, was able to refine the miss
distance uncertainty to within 137 m. In addition, NAVSPOC identified a minor perturbation in the orbit of Satellite 18208 which occurred about the time of the event.
Cosmos 2316-2318 Proton-K (4) fragments; 2 pieces, both have decayed.
This is the 4th breakup of 2000 and the 23rd breakup of a Proton SOZ motor (see Orbital Debris Quarterly Newsletter V, Issue 4, p. 2.) This object is associated with the 24 July 1995 launch (1995-037) of the Cosmos 2316-2318 satellites.
These members of the GLONASS series are equivalent to GPS/Navstar satellites and reside in middle Earth orbit. This object was one of two pieces left in the transfer orbit and is assessed to be one of the SOZ ullage/orientation motor units. As
of November 21, 2000, this object had been on orbit 5 years and 121 days.
D
1995-37 G
[23626]
1995 Jul 26
2 days
1995 Jul 27
Mugunghwa 1 fragment; 1 piece, it has decayed.
3 days
D
1995-37 H
[23627]
1995
1995
1995
1995
Jul
Jul
Jul
Jul
25.04
26.36
25.48
27.36
64.87
64.84
64.88
64.98
91.18
89.92
91.15
89.10
6712
6649
6709
6609
154
155
177
102
512
385
484
358
0.027
0.017
0.023
0.019
53
53
69
54
RAE Table of Earth Satellites
Year of Launch 1995
Cospar ID
[Norad number]
One piece was liberated. Event was 1995 Dec 6.
D 1995-41 D
[24310]
Descent date
Lifetime
2003 Jun 14
2870 days
Cosmos 2322 fragments; 4 pieces, 3 have decayed.
1995-58 G
[24284]
D
1995-58 H
[24455]
2001 Jan 22
1910 days
D
1995-58 J
[25905]
2000 Mar 9
1591 days
D
1995-58 K
[28293]
2005 Jul 4
3534 days
Bruno Beppi Rossi X-Ray Timing Explorer fragments; 3 pieces, 2 have decayed
D 1995-74 C
[23759]
1996 Jan 19
20 days
D
D
1995-74 D
1995-74 E
[23760]
[23761]
1996 Jan 5
1996 Jan 5
6 days
6 days
(Compiled 2006)
Nodal
period
(min)
Extra Page 1995 -3
Date of
orbital
Determination
Orbital
Inclination
(deg)
Semi
major axis
(km)
1996
2005
2010
1996
2001
1999
2000
2004
2005
2005
Aug
Feb
Dec
Sep
Jan
Sep
Mar
May
Feb
Jul
19.24
20.10
25.94
30.81
20.04
20.37
5.86
25.21
19.96
4.38
70.87
70.86
70.86
71.01
70.96
71.01
70.95
70.99
70.99
70.95
101.82
101.62
101.58
101.72
92.43
99.62
94.27
97.15
95.47
90.40
1996
1996
1996
1995
Jan
Jan
Jan
Dec
2.55
17.02
1.35
31.62
22.93
22.82
22.93
23.10
95.73
92.55
94.97
95.32
Perigee
height
(km)
Apogee
height
(km)
Orbital
eccentric.
Argument
of perigee
(deg)
7223
7213
7212
7219
6772
7119
6861
7001
6919
6672
834
825
825
831
378
732
466
619
532
276
855
844
842
849
409
748
500
625
549
311
0.001
0.001
0.001
0.001
0.002
0.001
0.002
0.0004
0.001
0.003
301
320
354
342
157
300
326
232
176
297
6932
6778
6896
6922
532
387
473
463
575
412
561
625
0.003
0.002
0.006
0.012
323
138
225
344