RAE Table of Earth Satellites
Year of Launch 1970
Name
[Launcher]
Fragments
Cospar ID
Launchdate
[Norad #] Launchsite Lifetime + Descent date
Cospar ID
[Norad]
(Revised 2002)
Shape and
weight (kg)
Descent date
Size
(m)
Lifetime
Date of
orbital
determination
Orbital
Inclination
(deg)
Nodal
period
(min)
Semi
major axis
(km)
Page 216
Perigee
height
(km)
Apogee
height
(km)
Orbital
Argument
eccentricity of perigee
(deg)
D
R
Cosmos 318
[Voskhod 11A57]
1970-01 A
[04292]
BAI
1970 Jan 9.39
11.90 days
1970 Jan 21.29
Spherecylinder
5700?
5.0 long
2.4 dia
1970 Jan l0.8
64.97
89.29
6618
203
277
0.006
31
D
Cosmos 318
Block I 3rd stage
197C-01 B
[04293]
1970 Jan 9.39
6.21 days
1970 Jan 15.60
Cylinder
2500?
7.5 long
2.6 dia
1970 Jan 10.7
64.97
89.11
6610
200
263
0.005
29
D
KH 8-25
[Titan 3B-25
Agena D]
1970-02 A
[04296]
VDB-SLC4W
1970 Jan 14.78
18 days
1970 Feb 1
Cylinder
3000?
8 long?
1.5 dia
1970 Jan 15.3
l00.96
89.69
6637
134
383
0.019
133
Intelsat 3 F-6
[Delta M 557 #75]
1970-03 A
[04297]
CC-LC17A
1970 Jan 15.01
> million years
Cylinder
293 full
137 empty
1.04 long
1.42 dia
1970
1970
1977
2002
28.C4
0.9
5.16
14.09
629.71
1436.1
1465.69
1452.27
24386
42165
42742
42481
267
35773
36185
36068
35748
3580l
36542
36137
0.727
0.0003
0.004
0.0008
181
- *
10
259
Intelsat 3 F-6
Star-37D PKM
1970-03 B
[04298]
1970 Jan 15.01
80 years
Sphere-cone
66
1.32 long
0.94 dia
1970 Jan 15.7
2002 Dec 13.65
28.04
27.73
629.70
488.63
24385
20550
267
297
35747
28047
0.727
0.675
181
244
D
Cosmos 319
[Kosmos 11K63]
1970-04 A
[04299]
PLE-LC133/1
1970 Jan 15.57
167.13 days
1970 Jul 1.70
Ellipsoid
400?
1.8 long
1.2 dia
1970 Jan 16.2
1970 Apr 1.0
51.96
81.96
102.03
98.97
7232
7088
200
195
1508
1224
0.090
0.073
74
-
D
Cosmos 319
rocket
1970-04 B
[04300]
1970 Jan 15.57
106.42 days
1970 May 1.99
Cylinder
1500?
8 long
1.65 dia
1970 Jan 16.2
81.96
101.85
7224
199
1493
0.090
74
*
Transmissions terminated after orbit change.
2014 – version 1.13
Jan
Feb
May
Dec
15.7
16.0
13.0
14.5
RAE Table of Earth Satellites
Year of Launch 1970
Name
[Launcher]
Fragments
Cospar ID
Launchdate
[Norad #] Launchsite Lifetime + Descent date
Cospar ID
[Norad]
(Revised 2002)
Shape and
weight (kg)
Descent date
Size
(m)
Lifetime
Date of
orbital
determination
Orbital
Inclination
(deg)
Nodal
period
(min)
Semi
major axis
(km)
Page 217
Perigee
height
(km)
Apogee
height
(km)
Orbital
Argument
eccentricity of perigee
(deg)
D
Cosmos 320
[Kosmos 11K63]
1970-05 A
[04301]
KY-LC86/4
1970 Jan l6.46
24.67 days
1970 Feb 10.13
Ellipsoid +
annular tall?
400?
6.5 long?
1.2 dia
1970 Jan 17.6
48.40
90.18
6665
247
326
0.006
139
D
Cosmos 320
rocket
1970-05 B
[04302]
1970 Jan 16.46
11.56 days
1970 Jan 28.02
Cylinder
1500?
8 long
1.65 dia
1970 Jan 18.5
48.41
90.19
6665
255
319
0.005
175
D
Fragments
1970-05 C-G
5 pieces, all have decayed
D
Cosmos 321 *
[Kosmos 11K63]
1970-06 A
[04308]
PLE-LC133/1
1970 Jan 20.85
61.39 days
1970 Mar 23.24
Ellipsoid
400?
1.8 long
1.2 dia
1970 Jan 93.9
70.95
92.07
6754
272
479
0.015
73
D
Comos 321
2nd stage
1970-06 B
[04309]
1970 Jan 20.85
45.56 days
1970 Mar 7.41
Cylinder
1500?
8 long
1.65 dia
1970 Jan 24.1
70.95
91.84
6742
270
458
0.014
72
D
D
Fragment
Fragment
1970-06 C
1970-06 D
[04313]
[04314]
1970 Jan 25
1970 Jan 29
5 days
9 days
D
R
Cosmos 322
[Voskhod 11A57]
1970-07 A
[04315]
PLE
1970 Jan 21.50
7.78 days
1970 Jan 29.28
Spherecylinder
5530?
5 long?
2.4 dia
1970 Jan 22.2
65.4l
89.65
6635
195
319
0.009
41
D
Cosmos 322
Block I 3rd stage
1970-07 B
[04316]
1970 Jan 21.50
4.33 days
1970 Jan 25.83
Cylinder
2500?
7.5 long
2.6 die
1970 Jan 22.2
65.40
89.46
6626
190
306
0.009
38
*
Ionospheric and geomagnetic stud ies.
2014 – version 1.13
For orbital information see extra pages at the end of the year
RAE Table of Earth Satellites
Year of Launch 1970
Name
[Launcher]
Fragments
Cospar ID
Launchdate
[Norad #] Launchsite Lifetime + Descent date
Cospar ID
[Norad]
Shape and
weight (kg)
Descent date
Size
(m)
Lifetime
Date of
orbital
determination
(Revised 2002)
Orbital
Inclination
(deg)
Nodal
period
(min)
Page 218
Semi
major axis
(km)
Perigee
height
(km)
Apogee
height
(km)
Orbital
Argument
eccentricity of perigee
(deg)
ITOS 1*
1970-08 A
(Tiros-M)
[04320]
[Delta N6 542 #76] VDB-SLC2W
1970 Jan 23.48
10000 years
Box + 3 panels 1.02 square 1970 Feb 14.3
309
1.22 long
2002 Dec 15.91
102.00
101.81
115.10
115.02
7837
7835
1436
1435
1482
1478
0.003
0.003
219
187
Oscar 5 #
(Australis)
1970-08 B
[04321]
1970 Jan 23.48
10000 years
Rectangular
box 18
0.43 x 0.30 1970 Jan 25.4
x 0.15
2002 Dec 15.79
101.96
101.85
115.08
115.00
7836
7834
1435
1434
1481
1477
0.003
0.003
263
174
ITOS 1
Delta N 2nd stage
1970-08 C
[04322]
1970 Jan 23.48
5000 years
Cylinder
350?
4.9 long
1.43 dia
1970 Jan 25.4
2002 Dec 18.54
101.95
101.88
115.11
115.02
7838
7835
1441
1435
1478
1479
0.002
0.003
262
196
SERT 2**
[Thorad 2L 534
Agena D (TA12)]
1970-09 A
[04327]
VDB-SLC2E
1970 Feb 4.12
800 years
Cylinder +
2 wings
1500
7.6 long
1.52 dia
12.2 span
1970
1970
1970
2002
99.13
99.13
99.13
99.18
105.15
106.94
106.23
106.03
7378
7458
7427
7421
997
1079
1045
1040
1003
1081
1052
1046
0.0004
0.0001
0.0005
0.0004
328
243
D
R
Cosmos 323
[Voskhod 11A57]
1970-10 A
[04328]
PLE
1970 Feb 10.50
7.78 days
1970 Feb 18.28
Spherecylinder
5530?
5 long?
2.4 dia
1970 Feb 11.2
65.43
89.65
6636
201
314
0.009
49
D
Cosmos 323
Block I 3rd stage
1970-10 B
[04329]
1970 Feb 10.50
5.08 days
1970 Feb 15.58
Cylinder
250Cr.P
7.5 lo@
2.6 dia
1970 Feb 12.2
65.41
89.27
6617
189
288
0.008
35
D
Ohsumi ##
[Lambda 4S #5]
1970-11 A
[04330]
KAG-L
1970 Feb 11.18
12225 days
2003 Aug 2
Cylinder
38
(payload 12)
1.00 long
0.48 dia
1970 Feb 14.7
2002 Dec 16.14
31.07
31.01
144.20
95.78
9117
6935
339
282
5138
832
0.263
0.039
131
99
* Improved Tiros Operational Satellite.
** Space Electric Rocket Test.
2014 – version 1.13
# Australian satellite
## Japanese satellite
Feb
Jul
Nov
Dec
11.8
23.0
1.0
22.50
RAE Table of Earth Satellites
Year of Launch 1970
Name
[Launcher]
Fragments
Cospar ID
Launchdate
[Norad #] Launchsite Lifetime + Descent date
Cospar ID
[Norad]
(Revised 2002)
Shape and
weight (kg)
Descent date
Size
(m)
Lifetime
Date of
orbital
determination
Orbital
Inclination
(deg)
Nodal
period
(min)
Semi
major axis
(km)
Page 219
Perigee
height
(km)
Apogee
height
(km)
Orbital
Argument
eccentricity of perigee
(deg)
DMSP B5A-01
[Thor Burner 2
# 287]
1970-12 A
[04331]
VDB-SLC10W
1970 Feb 11.36
80 years
12-faced
frustum
195
1.64 long
1.31 to
1.10 dia
1970 Feb 16.7
2002 Dec 15.54
98.71
99.02
101.39
100.63
7201
7167
773
746
874
832
0.007
0.006
12
208
Burner 2
rocket
1970-12 B
[04332]
1970 Feb 11.36
60 years
Sphere-cone
66
1.32 long
0.94 dla
1970 Feb 18.4
2002 Dec 15.78
98.74
98.84
101.38
100.73
7201
7172
772
750
874
838
0.007
0.006
7
330
D
Molniya-1 13
[Molniya 8K78M]
1970-13 A
[04336]
PLE
1970 Feb 19.79
2048 days
1975 Sep 29
Windmill +
6 vanes
1000?
3.4 long
1.6 dia
1970 Feb 26.2
1970 May 16.5
1973 Oct 16.5
65.44
65.57
65.1
703.13
717.73
717.95
26194
26556
26564
461
470
940
39170
39885
39426
0.739
0.742
0.724
285
-
D
Molniya-1 13
4th stage casing
1970-13 B
[04333]
1970 Feb 19.79
17.42 days
1970 Mar 9.21
Irregular
1970 Feb 20.6
65.42
91.43
6713
205
485
0.021
72
D
Molniya-1 13
Block I 3rd stage
1970-13 C
[04334]
1970 Feb 19.79
20.07 days
1970 Mar 11.86
Cylinder
25007
7.5
2.6
long
dia
1970 Feb 20.6
65.43
91.21
6713
220
449
0.017
70
D
Molniya-1 13
Block L 4th stage
1970-13 D
[04337]
1970 Feb 19.79
2150 days
1976 Jan 9
Cyllnder
440
2.0
2.0
long
dia
1970 Mar 2.0
1973 Oct 1.0
65.46
65.25
699.06
698.70
26093
26084
465
925
38964
38486
0.738
0.720
285
-
D
Cosmos 324
[Kosmos 11K63]
1970-14 A
[04338]
PLE-LC133/1
1970 Feb 27.73
84.53 days
1970 May 23.26
Ellipsoid
400?
1.8 long
1.2 dia
1970 Feb 28.4
71.03
91.97
6749
275
466
0.014
75
D
Cosmos 324
2nd stage
1970-14 B
[04339]
1970 Feb 27.73
42.75 days
1970 Apr 11.48
Cylinder
1500?
8 long
1.65 dia
1970 Mar 1.1
71.04
91.74
6737
277
441
0.012
73
2014 – version 1.13
RAE Table of Earth Satellites
Year of Launch 1970
Name
[Launcher]
Fragments
Cospar ID
Launchdate
[Norad #] Launchsite Lifetime + Descent date
Cospar ID
[Norad]
(Revised 2002)
Shape and
weight (kg)
Descent date
Size
(m)
Lifetime
Date of
orbital
determination
Orbital
Inclination
(deg)
Nodal
period
(min)
Semi
major axis
(km)
Page 220
Perigee
height
(km)
Apogee
height
(km)
Orbital
Argument
eccentricity of perigee
(deg)
D
R
Cosmos 325
[Voskhod 11A57]
1970-15 A
[04340]
PLE-LC43/4
1970 Mar 4.51
7.79 days
1970 Mar 12.30
Spherecylinder
5530?
5 long?
2.4 dia
1970 Mar 6.2
65.39
89.77
6642
200
327
0.010
49
D
Cosmos 325
2nd stage
1970-15 B
[04341]
1970 Mar 4.51
5.60 days
1970 Mar 10.11
cylinder
2500?
7.5 long
2.6 dia
1970 Mar 6.2
65.40
89.50
6628
194
306
0.008
39
D
Discoverer 135
(KH 4B-32)
[Thorad 2L 551
Agena D 1657]
1970-16 A
[04342]
VDB-SLC3W
1970 Mar 4.93
21.98 days
1970 Mar 26.91
Cylinder
2O00?
8 long?
1.5 dia
1970 Mar 5.6
88.02
88.76
6590
167
257
0.007
121
D
Hitchhiker 26 *
1970-16 B
[04343]
1970 Mar 4.93
615.19 days
1971 Nov 10.12
Octagon
60?
0.3 long?
0.9 dia?
1970 Mar 7.2
1970 Aug 31.7
1971 Apr 1.0
88.14
88.14
88.14
94.16
93.58
92.49
6856
6828
6773
442
420
376
514
479
414
0.005
0.004
0.003
10
-
D
DIAL/WIKA**
[Diamant B #1]
1970-17 A
[04344]
KOU-ELD
1970 Mar 10.51
3131 days
1978 Oct 5
Octagonal
door-knob
63
1.01 long
0.63 dia
1970 Mar 12.4
1971 Aug 1.0
5.44
5.44
104.20
102.14
7344
7247
301
304
1631
1434
0.091
0.078
112
-
D
DIAL / MIKA
Diamant B
3rd stage
1970-17 B
[04345]
1970 Mar 10.51
1644 days
1974 Sep 9
Cylinder
nozzle 120
(payload 52)
2.60 long
0.80 dia
1970 Mar
1971 Feb
1972 Oct
11.7
1.0
1.0
5.42
5.42
5.42
104.67
102.49
99.20
7367
7264
7108
313
303
293
1665
1468
1166
0.092
0.080
0.061
105
-
D
R
Cosmos 326
[Voskhod 11A57]
1970-18 A
[04346]
PLE-LC43/4
1970 Mar 13.34
7.88 davs
1970 Mar 21.22
Spherecylinder
5533?
5 long?
2.4 dia
1970 Mar
13.8
81.35
90.20
6661
2Q3
363
0.012
85
D
Cosmos 326
Block I 3rd stage
1970-18B
[04347]
1970 Mar 13.34
8.98 days
1970 Mar 23.32
Cylinder
2500?
7.5 long
2.6 dia
1970 Mar
14.3
81.36
90.00
6651
202
346
0.011
83
* 1970-16 B ejected from 1970-16 A on 1970 Mar 5.00.
** Dlamant B - ALlemand (French-German satellite).
2014 – version 1.13
RAE Table of Earth Satellites
Year of Launch 1970
Name
[Launcher]
Fragments
Cospar ID
Launchdate
[Norad #] Launchsite Lifetime + Descent date
Cospar ID
[Norad]
(Revised 2002)
Shape and
weight (kg)
Descent date
Size
(m)
Lifetime
Date of
orbital
determination
Orbital
Inclination
(deg)
Nodal
period
(min)
Semi
major axis
(km)
Page 221
Perigee
height
(km)
Apogee
height
(km)
Orbital
Argument
eccentricity of perigee
(deg)
D
Meteor-1 3
[Vostok 8A92M]
1970-19 A
[04349]
PLE
1970 Mar 17.47
4994 days
1983 Nov 18
Cylinder +
2 vanes
2200?
5 1ong?
1.5 dia?
1970 Mar 18.2
81.18
96.42
6964
537
635
0.007
236
D
Meteor-1 3
Block E 3rd stage
1970-19 B
[04350]
1970 Mar 17.47
4637 days
1982 Nov 26
Cylinder
1440
3.8 long
2.6 dia
1970 Mar 18.8
81.17
96.55
6971
467
718
0.018
205
D
Fragment
1970-19 C
[05573]
1974 Nov 3
1692 days
D
Cosmos 327
[Kosmos 11K63]
1970-20 A
[04351]
PLE-LC133/1
1970 Mar 18.61
306.41 days
1971 Jan 19.02
Ellipsoid
400?
1.8 long
1.2 dia
1970 Mar 19.6
1970 Aug 31.7
70.95
70.95
95.65
93.64
6928
6832
280
255
819
652
0.033
0.029
87
-
D
Cosmos 327
2nd stage
1970-2O B
[04352]
1970 Mar 18.61
192.44 days
1970 Sep 27.05
Cylinder
1500?
8 long
1.65 dia
1970 Mar 19.6
1970 Jul 1.3
70.94
70.94
95.57
93.39
6924
6819
272
254
819
628
0.039
0.027
85
-
NAT0 1 *
[Delta M 558 #77]
1970-21 A
[04353]
CC-LC17A
1970 Mar 20.99
> million
years
Cylinder
243 full
117 empty
0.81 long
1.37 dia
1973
1970
1975
2002
21.0
1.0
1.0
19.03
25.81
2.8
1.7
13.71
656.9
1403.4
1436.3
1436.17
25043
41523
42168
42166
281
34429
35745
35773
37048
35860
35834
35802
0.734
0.017
0.001
0.0003
179
40
NATO 1
Star-37D PKM
1970-21 B
[04354]
1970 Mar 20.99
100 years
Sphere-cone
66
1.32 long
0.94 dia
1970 Mar 21.3
2002 Dec 13.15
25.67
25.19
655.4
474.87
24993
20163
295
310
36934
27259
0.733
0.668
179
297
Fragment
1970-21 C
[05975]
2002 Dec 16.21
25.59
500.63
20885
315
28699
0.680
221
D
R
Cosmos 328 **
[Voskhod 11A57]
1970-22 A
[04355]
PLE
1970 Mar 27.49
12.77 days
1970 Apr 9.26
Spherecylinder
630
6.5 long?
2.4 dia
1970 Mar 28.6
1970 Mar 29.8
72.86
72.86
89.54
89.75
6629
6639
203
206
299
316
0.007
0.008
56
59
D
Cosmos 328
Block I 3rd stage
1970-22 B
[04356]
1970 Mar 27.49
4.69 days
1970 Apr 1.18
Cylinder
2500?
7.5 long
2.6 dia
1970 Mar 28.4
72.87
89.39
6622
204
284
0.006
53
* North Atlantic Treaty Organisation
** Cosmos 328 manoeuvred, but no jettisoned engine was tracked or des ignated
2014 – version 1.13
Mar
May
May
Dec
RAE Table of Earth Satellites
Year of Launch 1970
Name
[Launcher]
Fragments
Cospar ID
Launchdate
[Norad #] Launchsite Lifetime + Descent date
Cospar ID
[Norad]
(Revised 2002)
Shape and
weight (kg)
Descent date
Size
(m)
Lifetime
Date of
orbital
determination
Orbital
Inclination
(deg)
Nodal
period
(min)
Semi
major axis
(km)
Page 222
Perigee
height
(km)
Apogee
height
(km)
Orbital
Argument
eccentricity of perigee
(deg)
D
R
Cosmos 329
[Voskhod 11A57]
1970-23 A
[04357]
PLE
1970 Apr 3.36
11.87 days
1970 Apr 15.23
spherecylinder
5700?
5.0 long
2.4 dia
1970 Apr 4.1
81.33
88.79
6591
198
228
0.002
319
D
Cosmos 329
Block I 3rd stage
1970-23 B
[04358]
1970 Apr 3.36
2.44 days
1970 Apr 5.80
Cylinder
2500?
7.5 long
2.6 dia
1970 Apr 4.3
81.32
88.52
6578
185
214
0.002
316
D
Cosmos 330
[Kosmos 11K65M]
1970-24 A
[04360]
PLE-LC132
1970 Apr 7.47
3353 days
1979 Jun 12
Cylinder +
paddles?
900?
2 long?
1 dia?
1970 Apr 8.6
1970 Sep 16.0
74.06
74.06
95.22
94.63
6907
6878
514
492
543
508
0.002
0.001
334
-
D
Cosmos 330
2nd stage
1970-24 B
[04361]
1970 Apr 7.47
3504 days
1979 Nov 10
Cylinder
2200?
7.4 long
2.4 dla
1970 Apr 10.2
1973 Feb 1.0
74.06
74.06
95.12
94.56
6902
6875
507
480
541
513
0.002
0.002
336
-
1970 Apr 8.35
1200 years
Conical
skeleton +
3.00 long
1.45 dia
2 paddles
1970 Apr 10.2
2002 Dec 18.05
99.89
100.07
107.29
107.12
7476
7471
1064
1088
1100
1098
0.003
0.0007
8
278
Nimbus 4
1970-25 A
[Thorad 2L 553
[04362]
Agena D 6223(TA13)] VDB-SLC2E
620
TOPO 1
(S70-3)
1970-25 B
[04363]
1970 Apr 8.35
2000 years
Rectangular
box
18
0.36 x 0.30 1970 Apr 9.5
x 0.23
2002 Dec 15.89
99.76
99.97
107.09
106.95
7466
7464
1064
1084
1111
1087
0.003
0.0002
193
32
Nimbus 4
Agena D stage
1970-25 C
[04367]
1970 Apr 8.35
1000 years
Cylinder*
700?
6 long?
1.5 dia
99.89
99.49
106.86
104.85
7454
7366
1066
971
1086
1005
0.001
0.002
331
322
Fragments
1970-25 D-QT
D
R
Cosmos 331
[Voskhod 11A57]
1970-26 A
[04364]
BAI
1970 Apr 8.43
7.92 days
1970 Apr 16.35
Spherecylinder
5530?
5 long?
2.4 dia
1970 Apr 10.2
65.02
89.77
6641
206
320
0.009
45
D
Cosmos 331
Block I 3rd stage
1970-26 B
[04365]
1970 Apr 8.43
7.80 days
1970 Apr 16.23
Cylinder
2500?
7.5 long
2.6 dla
1970 Apr 10.1
65.01
89.60
6633
205
305
0.007
43
375 pieces, 125 have decayed
Before explosion about 1970 Nov 4.
2014 – version 1.13
1970 Apr 10.2
2002 Dec 15.77
For orbital information see extra pages at the end of the year
RAE Table of Earth Satellites
Year of Launch 1970
Name
[Launcher]
Fragments
Cospar ID
Launchdate
[Norad #] Launchsite Lifetime + Descent date
Cospar ID
[Norad]
Shape and
weight (kg)
Descent date
(Revised 2002)
Size
(m)
Lifetime
Date of
orbital
determination
Orbital
Inclination
(deg)
Nodal
period
(min)
Semi
major axis
(km)
Perigee
height
(km)
Page 223
Apogee
height
(km)
Orbital
Argument
eccentricity of perigee
(deg)
Ve1a 11
[Titan 3C-18]
1970-27 A
[04366]
CC-LC40
1970 Apr 8.46
Icosahedron
> million years ## 259
1.27 dia
1970 Apr 9.4
1984 Sep 1.00
32.41
31.17
6729
6690.98
118060 111210 112160 0.005
117621 101260 121225 0.085
280
83
Vela 12
1970-27 B
[04368]
1970 Apr 8.46
Icosahedron
> million years ## 259
1.27 dia
1970 Apr 11.6
1983 Jan 3.00
32.52
57.35
6745
6707.90
118230 111500 112210 0.003
117819 103569 119312 0.067
47
79
Vela 11
Titan 3C stage
1970-27 C
[NNA]
1970 Apr 8.46
> million years
Cylinder
1500?
6 long?
3.0 dia
1970 Apr 10.4
32.36
3005
68980
l504O
110170 0.690
178*
Cosmos 332
[Kosmos 11K65M]
1970-28 A
[04369]
PLE-LC132
1970 Apr 11.71
100 years
Cylinder
paddles
750?
2 long?
1 dia?
1970 Apr 12.4
2002 Dec 17.93
74.05
74.03
100.01
99.32
7136
7104
755
722
761
730
0.0004
0.0005
110
57
Cosmos 332
2nd stage
1970-28 B
[04370]
1970 Apr 11.71
80 years
Cylinder
2200?
7.4 long
2.4 dia
1970 Apr 12.4
2002 Dec 17.78
74.05
74.03
99.90
98.83
7131
7081
744
691
762
715
0.001
0.002
34
267
Fragment
1970-28 C
[14814]
2005 Oct 15
12971 days
2002 Dec 17.21
2005 Oct 15.23
74.01
73.97
95.53
88.13
6923
6560
540
173
550
190
0.0008
0.001
251
154
D Apollo l3**
3M [Saturn 508]
R
1970-29 A
[04371]
CC-LC39A
1970 Apr 11.80
5.95 days
1970 Apr 17.75
Conecylinder
28890
11.15 long
3.91 dia
1970 Apr 11.8
32.56
88.07
6564
186
1970 Apr 12.0
33.2
26320
292520 200
Passed 252 km beyond Moon 197O Apr 15.02
Landend on earth 1970 Apr 17 at 18:07.
186
0
572080 0.977
-*
30*
D
Saturn IVB
1970-29 B
[04372]
1970 Apr 11.80
3.25 days
1970 Apr 15.05
Cylinder
13930
18.7 long
6.6 dla
1970 Apr 11.8
32.56
88.07
6564
186
186
0
1970 Apr 12.0
33.2
26320
292520 200
572080 0.977
Crashed on Moon Apr 15 at 01:09. Impact: 2.4S, 27.9W
-*
30*
D
LEM 7#
1970-29 C
1970 Apr 11.80
Box + octa-
4.1 high
1970 Apr 12.0
30*
[NNA]
5.95 days
1970 Apr 17.75
gon + 4 legs
15l90, then
7890
3.76 wide
3.13 deep
Passed 252 km beyond Moon 197 Apr 15.02.
Decayed in Earth's atmosphere 1970 Apr 17 at 17:57.
D
*
**
#
##
Aproxlmate orbits.
Apollo attached to LEM, separated from Saturn IVB on Apr 11.98.
Apollo command module jettisoned service module on Apr 17.55; and jettisoned LEM on Apr 17.70.
Admistratily decayed by Norad on 1993 Jan 1, but still in orbit.
2014 – version 1.13
33.2
26320
292520 200
572080 0.9777
RAE Table of Earth Satellites
Year of Launch 1970
Name
[Launcher]
Fragments
Cospar ID
Launchdate
[Norad #] Launchsite Lifetime + Descent date
Cospar ID
[Norad]
(Revised 2002)
Shape and
weight (kg)
Descent date
Size
(m)
Lifetime
Date of
orbital
determination
Orbital
Inclination
(deg)
Nodal
period
(min)
Semi
major axis
(km)
Page 224
Perigee
height
(km)
Apogee
height
(km)
Orbital
Argument
eccentricity of perigee
(deg)
D
R
Cosmos 333
[Voskhod 11A57]
1970-30 A
[04373]
PLE
1970 Apr 15.38
12.85 days
1970 Apr 26.23
Spherecylinder
6300?
6.5 long?
2.4 dia
1970 Apr 15.6
81.34
89.11
6607
219
239
0.001
80
D
Cosmos 333
Block I 3rd stage
1970-30 B
[04374]
1970 Apr 15.38
3.20 days
1970 Apr 18.58
Cylinder
2500?
7.5 long
2.6 dia
1970 Apr 15.7
81.36
88.99
6601
213
233
0.002
8
D
Cosmos 333
Engine *
1970-30 C
[04395]
1970 Apr 15.38
16.64 days
1970 May 2.02
Cone
600? full
1.5 long?
2 die?
1970 Apr 28.2
81.34
88.66
6585
195
218
0.002
331
D
Fragment
1970-30 D
[04396]
D
KH 8-26
[Titan 3B-26
Agena D
1970-31 A
[04375]
VDB-SLC4W
1970 Apr 15.66
21 days
1970 May 6
Cylinder
3000?
8 1ong
1.5 dia
1970 Apr 16.6
1970 Apr 24.3
110.97
l10.96
89.70
89.91
6637
6648
130
131
388
408
0.019
0.021
120
121
Intelsat 3-7
[Delta M 559 #78]
1970-32 A
[04376]
CC-LC17A
1970 Apr 23.03
million
years
Cylinder
293 full
137 empty
1.04 long
1.42 dia
1970 May 17.9
1971 May 25.00
2009 Mar 13.41
0.21
0.85
10.34
1436.2
1435.92
1435.80
42167
42161
42159
35772
35775
35727
35805
35791
35834
0.0004
0.0002
0.001
345
157
285 &
Intelsat 3-7
Star-37D PKM
1970-32 B
[04377]
1970 Apr 23.03
40 years
Sphere-cone
66
1.32 long
0.94 dia
1970 Apr 23.7
1971 Dec 1.0
2002 Dec 16.07
28.04
28.1
26.88
643.2
629.5
396.90
24682
24329
17890
272
193
307
36336
35708
22717
0.731
0.730
0.626
181
40
D
Cosmos 334 #
[Kosmos 11K63]
1970-33 A
[04378]
PLE-LC133/1
1970 Apr 23.56
108.39 days
1970 Aug 9.95
Ellipsoid
400?
1.8 long
1.2 dia
1970 Apr 24.2
70.92
92.10
6755
272
482
0.0l6
81
D
Cosmos 334
2nd stage
1970-33 B
[04379]
1970 Apr 23.56
23.05 days
1970 May 16.61
Cylinder
1500?
8 long
1.65 dia
1970 Apr 24.3
70.92
91.95
6748
249
491
0.018
76
D
D
D
Fragment
Fragment
Fragment
1970-33 C
1970-33 D
1970-33 E
[04397]
[04398]
[04399]
1970 Jul 8
1970 May 25
1970 May 16
76 days
32 days
23 days
*
#
&
1970-30 C ejected from 1970-30 A about 1970 Apr 28.2.
Analyses indicate that the Cosmos 334 payload is the most likely debris source.
Orbit from amateur observations.
2014 – version 1.13
RAE Table of Earth Satellites
Year of Launch 1970
Name
[Launcher]
Fragments
Cospar ID
Launchdate
[Norad #] Launchsite Lifetime + Descent date
Cospar ID
[Norad]
(Revised 2002)
Shape and
weight (kg)
Descent date
Size
(m)
Lifetime
Date of
orbital
determination
Orbital
Inclination
(deg)
Nodal
period
(min)
Semi
major axis
(km)
Page 225
Perigee
height
(km)
Apogee
height
(km)
Orbital
Argument
eccentricity of perigee
(deg)
China 1
[CZ-1]
1970-34 A
[04382]
JIUQ
1970 Apr 24.57
100 years
Spheroid
173
1 dia?
1970 Apr 27.7
2002 Dec 16.53
68.44
68.42
114.09
110.75
7792
7640
441
435
2386
2088
0.125
0.108
141
49
D
China 1
3rd stage
1970-34 B
[04392]
1970 Apr 24.57
11206.67 days
2000 Dec 29.24
Cylinder
-
1970 Apr 30.0
68.45
114.09
7792
441
2386
0.125
139
D
Fragment
Fragment
1970-34 C
1970-34 D
[04400]
[25882]
1983 Mar 23
4716 days
2002 Dec 20.11
68.39
106.70
7452
428
1720
0.087
105
D
Cosmos 335*
[Kosmos 11K63]
1970-35 A
[04380]
KY-LC86/4
1970 Apr 24.94
58.15 days
1970 Jun 22.09
Ellipsoid
400?
1.8 long
1.2 dia
1970 Apr 25.5
48.40
90.97
6704
250
401
0.011
127
D
Cosmos 335
2nd stage
1970-35 B
[04381]
1970 Apr 24.94
22.72 days
1970 May 17.66
Cylinder
1500?
8 long
1.65 dia
1970 Apr 25.5
48.44
90.88
6699
250
392
0.011
127
Cosmos 336 **
[Kosmos 11K65M]
1970-36 A
[04383]
PLE-LC132
1970 Apr 25.71
10000 years
Spheroid
40?
1.0 long?
0.8 dia?
1970 Apr 30.2
2002 Dec 15.96
74.04
74.03
115.49
115.42
7855
7853
1464
1464
1490
1486
0.002
0.001
199
20
Cosmos 337 **
1970-36 B
[04384]
1970 Apr 25.71
10000 years
Spheroid
40?
1.0 long?
0.8 dia?
1970 Apr 27.1
2002 Dec 16.22
74.05
74.03
116.27
116.20
7890
7889
1470
1468
1554
1553
0.005
0.005
258
346
Cosmos 338 **
1970-36 C
[04385]
1970 Apr 25.71
10000 years
Spheroid
40?
1.0 long?
0.8 dia?
1970 Apr 28.6
2002 Dec 15.93
74.03
74.03
115.89
115.82
7873
7871
1472
1467
1518
1518
0.003
0.003
250
206
Cosmos 339 **
1970-36 D
[04386]
1970 Apr 25.71
9000 years
Spheroid
40?
1.0 long?
0.8 dia?
1970 Apr 30.2
2002 Dec 15.71
74.04
74.03
115.10
115.03
7837
7835
1446
1445
1472
1469
0.002
0.001
1ll
141
Cosmos 340 **
1970-36 E
[04387]
1970 Apr 25.71
8000 years
Spheroid
40?
1.0 long?
0.8 dia?
1970 Apr 2.2
2002 Dec 15.74
74.04
74.02
114.70
114.62
7819
7817
1409
1408
1473
1469
0.004
0.004
100
344
* Ultra-violet radiation studies.
** Strela-1M
2014 – version 1.13
1970-36 continued on page 226
RAE Table of Earth Satellites
Year of Launch 1970
Name
[Launcher]
Fragments
Cospar ID
Launchdate
[Norad #] Launchsite Lifetime + Descent date
Cospar ID
[Norad]
(Revised 2002)
Shape and
weight (kg)
Descent date
Size
(m)
Lifetime
Date of
orbital
determination
Orbital
Inclination
(deg)
Nodal
period
(min)
Page 226
Semi
major axis
(km)
Perigee
height
(km)
Apogee
height
(km)
Orbital
Argument
eccentricity of perigee
(deg)
Cosmos 341 **
1970-36 F
[04388]
1970 Apr 25.71
6000 years
Spheroid
40?
1.0 long?
0.8 dia?
1970 Apr 27.3
2002 Dec 15.67
74.04
74.03
113.97
113.90
7786
7784
1345
1343
1471
1468
0.008
0.008
98
64
Cosmos 342 **
1970-36 G
[04389]
1970 Apr 25.71
5000 years
Spheroid
40?
1.0 long?
0.8 dia?
1970 Apr 27.3
2002 Dec 15.95
74.04
74.02
113.62
113.53
7770
7767
1313
1310
1471
1468
0.010
0.010
94
282
Cosmos 343 **
1970-36 H
[04390]
1970 Apr 25.71
7000 years
Spheroid
40?
1.0 long?
0.8 dia?
1970 May 1.7
2002 Dec 15.93
74.02
74.02
114.32
115.25
7802
7800
1374
1375
1474
1468
0.006
0.006
97
194
Cosmos 336-343
2nd stage
1970-36 J
[04391]
1970 Apr 25.71
20000 years
Cylinder
2200?
7.4 long
2.4 dia
1970 May 3.l
2002 Dec 17.94
74.04
74.02
116.69
116.60
7910
7906
1473
1468
1590
1588
O.O07
0.008
257
130
Meteor-1 4
[Vostok 8A92M]
1970-37 A
[04393]
PLE
1970 Apr 28.45
12376 days
2004 Mar 16
Cylinder +
2 vanes
2200?
5 long?
1.5 dia?
1970 Apr 29.5
2002 Dec 22.38
81.23
81.17
98.12
93.00
7O46
6800
625
411
710
432
0.006
0.002
89
357
Meteor-1 4
Block E 3rd stage
1970-37 B
[04394]
1970 Apr 28.45
60 years
Cylinder
1440
3.8 long
2.6 dia
1970 May 4.1
2002 Dec 22.56
81.24
81.21
98.34
95.60
7056
6926
571
496
785
600
0.015
0.007
136
169
D
Fragment
1970-37 C
[05055]
D
R
Cosmos 344
[Voskhod 11A57]
1970-38 A
[04401]
PLE-LC41/1
1970 May 12.43
7.85 days
1970 May 20.28
Spherecylinder
5530?
5 long?
2.4 dia
1970 May 13.2
72.90
99.83
6644
202
329
0.010
45
D
Cosmos 344
Block I 3rd stage
1970-38 B
[04402]
1970 May 12.43
7.61 days
1970 May 20.04
Cylinder
2500?
7.5 long
2.6 dia
1970 May 13.2
72.90
89.65
6635
204
309
O.O08
34
D
** Strela-1M
2014 – version 1.13
RAE Table of Earth Satellites
Year of Launch 1970
Name
[Launcher]
Fragments
Cospar ID
Launchdate
[Norad #] Launchsite Lifetime + Descent date
Cospar ID
[Norad]
(Revised 2002)
Shape and
weight (kg)
Descent date
Size
(m)
Lifetime
Date of
orbital
determination
Orbital
Inclination
(deg)
Nodal
period
(min)
Semi
major axis
(km)
Page 227
Perigee
height
(km)
Apogee
height
(km)
Orbital
Argument
eccentricity of perigee
(deg)
D
Cosmos 345
[Voskhod 11A57]
1970-39 A
[04403]
BAI
1970 May 20.39
7.98 days
1970 May 28.37
Spherecylinder
5530?
5 long
2.4 dia
1970 May 21.5
51.75
89.06
6609
192
270
0.006
13
D
Cosmos 345
Block I 3rd stage
1970-39 B
[04404]
1970 May 20.39
2.70 days
1970 May 23.09
Cylinder
2500?
7.5 long
2.6 dia
1970 May 20.8
51.76
88.97
6605
185
268
0.006
0
D
Discoverer 136
(KH 4B-23)
[Thorad 2L 555
Agena D 1656]
1970-40 A
[04405]
VDB-SLC3W
1970 May 20.90
27.53 days
1970 Jun 17.43
Cylinder
2000?
8 long?
1.5 dia
1970 May 22.2
83.OO
88.62
6583
162
247
0.006
141
D
Doppler Beacon 2*
(Hitchhiker 27)
1970-40 B
[04406]
1970 May 20.90
1387.24 days
1974 Mar 8.14
Octagon?
60?
0.3 long?
0.9 dla?
1970 May 22.4
1971 Jul 1.0
1973 Feb 1.0
83.12
83.12
83.12
94.59
93.92
92.61
6875
6843
6779
491
460
397
503
469
405
0.0009
O.O007
0.0006
61
-
D Soyuz 9
2M [Soyuz 11A511]
R
1970-41 A
[04407]
BAI-LC1
1970 Jun 1.79
17.71 days
1970 Jun 19.50
Spherecylinder
+ 2 wings
6500
7.5 long
2.2 dia
1970 Jun 2.0
1970 Jun 2.2
1970 Jum 3.5
51.64
51.66
51.67
88.47
89.06
89.48
6580
6609
6630
176
208
244
227
254
259
0.004
0.003
0.001
166
125
213
D
Soyuz 9
Block I 3rd stage
1970-41 B
[04408]
1970 Jun 1.79
1.83 days
1970 Jun 3.62
Cylinder
2500?
7.5 long
2.6 dia
1970 Jun 2.2
51.67
88.36
6574
194
198
0.0003
353
D
R
Cosmos 346
[Voskhod 11A57]
1970-42 A
[04409]
BAI
1970 Jun 10.40
7.00 days
1970 Jun 17.40
Spherecylinder
5530?
5 long?
2.4 dia
1970 Jun 14.0
51.74
89.16
6614
197
274
0.006
36
D
Cosmos 346
Block I 3rd stage
1970-42 B
[04410]
1970 Jun 10.40
3.51 days
1970 Jun 13.91
Cylinder
2500?
7.5 long
2.6 dia
1970 Jun 14.6
51.74
88.46
6580
167
236
0.005
352
*
1970-40 B ejected from 1970-40 A about 1970 May 20.97.
2014 – version 1.13
RAE Table of Earth Satellites
Year of Launch 1970
Name
[Launcher]
Fragments
Cospar ID
Launchdate
[Norad #] Launchsite Lifetime + Descent date
Cospar ID
[Norad]
(Revised 2002)
Shape and
weight (kg)
Descent date
Size
(m)
Lifetime
Date of
orbital
determination
Orbital
Inclination
(deg)
Nodal
period
(min)
Semi
major axis
(km)
Page 228
Perigee
height
(km)
Apogee
height
(km)
Orbital
Argument
eccentricity of perigee
(deg)
D
Cosmos 347
[Kosmos 11K63]
1970-43 A
[04411]
KY-LC86/4
1970 Jun 12.40
513.18 days
1971 Nov 7.58
Ellipsoid
400?
1.8 long
1.2 dia
1970 Jun 15.5
1970 Dec 1.0
1971 May 16.5
48.41
48.3
48.3
107.9O
103.60
98.20
75ll
7310
7054
216
213
204
2050
1650
1148
0.122
0.098
0.067
110
-
D
Cosmos 347
2nd stage
1970-43 B
[04412]
1970 Jun 12.40
247.51 days
1971 Feb 14.91
Cylinder
1500?
8 long
1.65 dia
1970 Jun 15.5
1970 Oct 1.0
48.41
48.37
107.77
103.56
7505
7308
215
209
2039
1650
0.121
0.099
110
-
D
Cosmos 348*
[Kosmos 11K63]
1970-44 A
[04413]
PLE-LC133/1
1970 Jun 13.21
41.88 days
1970 Jul 25.09
Ellipsoid
400?
1.8 long
1.2 dla
1970 Jun 13.9
70.99
93.10
6804
201
651
0.033
90
D
Cosmos 348
2nd stage
l970-44 B
[04414]
1970 Jun 13.21
25.88 days
1970 Jul 9.09
Cylinder
1500?
8 long
1.65 dia
1970 Jun 15.5
70.98
92.78
6788
201
619
0.031
88
D
Fragment
1970-44 C
[04415]
1970 Jun 17
4 days
D
R
Cosmos 349
[Voshod 11A57]
1970-45 A
[04416]
PLE
1970 Jun 17.54
7.79 days
1970 Jun 25.33
Spherecylinder
5530?
5 long?
2.4 dia
1970 Jun 18.0
65.39
89.81
6644
199
332
0.010
46
D
Cosmos 349
rocket
1970-45 B
[04417]
1970 Jun 17.54
5.33 days
1970 Jun 22.87
Cylinder
2500?
7.5 long
2.6 dla
1970 Jun 17.8
65.40
89.67
6637
191
326
0.0l0
42
D
BMEWS 3
1970-46 A
(Rhyolite 1)
[04418]
[Atlas SLV-3A
CC-LC13
5201 A Agena D 1551]
1970 Jun 19.48
12 years?
Cylinder
700 full?
1.7 long?
1.4 dia?
1970 Jul 15.2
29.21
588.85
23310
178
33685
0.719
197
D
Rhyolite 1
Agena D
1970 Jun 19.48
12 years?
Cylinder
700?
6 long?
1.5 dia
1970 Sep 1.4
1972 Jul 1.0
1975 Mar 1.0
27.98
28.4
28.06
579.51
508.1
445.4
23041
21106
19317
171
194
224
33154
29262
25654
0.716
0.689
0.658
230
-
*
International atmospheric and auroral studies.
2014 – version 1.13
1970-46 B
[04511]
RAE Table of Earth Satellites
Year of Launch 1970
Name
[Launcher]
Fragments
Cospar ID
Launchdate
[Norad #] Launchsite Lifetime + Descent date
Cospar ID
[Norad]
(Revised 2002)
Shape and
weight (kg)
Descent date
Size
(m)
Lifetime
Date of
orbital
determination
Orbital
Inclination
(deg)
Nodal
period
(min)
Semi
major axis
(km)
Page 229
Perigee
height
(km)
Apogee
height
(km)
Orbital
Argument
eccentricity of perigee
(deg)
Meteor-1 5
[Vostok 8A92M]
1970-47 A
[04419]
PLE
1970 Jun 23.60
400 years
Cylinder +
2 vanes
2200?
5 1on9?
1.5 dia?
1970 Jun 25.3
2002 Dec 17.85
81.23
81.22
102.16
101.78
7238
7222
831
814
888
873
0.004
0.004
248
54
Meteor-1 5
Block E 3rd stage
1970-47 B
[04420]
1970 Jun 23.60
300 years
Cylinder
1440
3.8 long
2.6 dia
1970 Jun 27.1
2002 Dec 17.88
81.23
81.23
102.34
102.02
7246
7233
810
791
926
918
0.008
0.009
189
144
D
KH 8-27
[Tltan 3B-27
Agena D]
1970-48 A
[04422]
VDB-SLC4W
1970 Jun 25.62
11 days
1970 Jul 6
Cylinder
3000?
8 long?
1.5 dla
1970 Jun 26.9
1970 Jun 28.7
106.87
108.87
89.70
89.74
6637
6639
129
128
389
394
0.020
0.020
118
119
D
Molniya-1 14
[Molniya 8K78M]
1970-49 A
[04430]
PLE
1970 Jun 26.14
2061 days
1976 Feb 16
Windmill
6 vanes
1000?
3.4 long
1.6 dia
1970 Jun 7.5
1970 Aug 1.0
1973 Feb 1.0
65.37
65.34
65.45
704.70
717.55
717.43
26232
26551
26548
448
473
1531
39260
39872
38808
0.740
0.742
0.702
285
-
D
Molniya-1 14
4th stage casing
1970-49 B
[04424]
1970 Jun 26.14
29.54 days
1970 Jul 25.68
Irregular
-
-
1970 Jun 27.7
65.40
91.40
6722
225
462
0.018
69
D
Molniya-1 14
Block I 3rd stage
1970-49 C
[04423]
1970 Jun 26.14
21.70 days
1970 Jul 17.84
Cylinder
2500?
7.5 long
2.6 dia
1970 Jun 27.7
65.39
91.30
6717
213
464
0.019
63
D
Molniya-1 14
Block L 4th stage
1970-49 D
[04431]
1970 Jun 26.14
2076 days
1976 Mar 2
Cylinder
440
2.0 long
2.0 dia
1970 Jul 8.4
1973 Feb 1.0
65.39
65.43
700.30
700.30
26123
26123
469
1479
39021
38011
0.738
0.699
285
-
D
R
Cosmos 350
[Voskhod 11A57]
1970-50 A
[04425]
BAI
1970 Jun 26.50
11.93 days
1970 Jul 8.43
Spherecylinder
5700?
5.0 long
2.4 dia
1970 Jun 27.5
51.73
89.04
6608
202
258
0.004
26
D
Cosmos 350
Block I 3rd stage
1970-50 B
[04426]
1970 Jun 26.50
2.61 days
1970 Jun 29.11
Cylinder
25O0?
7.5 long
2.6 dia
1970 Jun 26.9
51.74
88.87
6600
190
253
0.005
9
2014 – version 1.13
RAE Table of Earth Satellites
Year of Launch 1970
Name
[Launcher]
Fragments
Cospar ID
Launchdate
[Norad #] Launchsite Lifetime + Descent date
Cospar ID
[Norad]
(Revised 2002)
Shape and
weight (kg)
Descent date
Size
(m)
Lifetime
Date of
orbital
determination
Orbital
Inclination
(deg)
Nodal
period
(min)
Semi
major axis
(km)
Page 230
Perigee
height
(km)
Apogee
height
(km)
Orbital
Argument
eccentricity of perigee
(deg)
D
Cosmos 351
[Kosmos 11K63]
1970-51 A
[04427]
PLE-LC133/1
1970 Jun 27.32
108.15 days
1970 Oct 13.47
Ellipsoid
400?
1.8 long
1.2 dia
1970 Jun 29.4
70.99
91.93
6747
270
467
0.015
82
D
Cosmos 351
2nd stage
1970-51 B
[04428]
1970 Jun 27.32
52.2 days
1970 Aug 18.5
Cylinder
1500?
8 long
1.65 dia
1970 Jun 28.5
70.98
91.75
6738
270
450
0.013
81
D
R
Cosmos 352
[Voskhod 11A57]
1970-52 A
[04446]
BAI
1970 Jul 7.44
7.95 days
1970 Jul 15.39
Spherecylinder
5530?
5 long?
2.4 dia
1970 Jul 8.2
51.78
89.46
6629
207
294
0.007
51
D
Cosmos 352
Block I 3rd stage
1970-52 B
[04447]
1970 Jul 7.44
4.59 days
1970 Jul 12.03
Cylinder
2500?
7.5 long
2.6 dia
1970 Jul 8.3
51.77
89.33
6622
187
301
0.009
32
D
Cosmos 353
1970-53 A
1970 Jul 9.57
Sphere-
5.0 long
1970 Jul 11.2
65.42
89.38
6622
204
284
0.006
58
R
[Voskhod 11A57]
[04477]
PLE
11.72 days
1970 Jul 21.29
cylinder
5700?
2.4 dia
D
Cosmos 353
Block I 3rd stage
1970-53 B
[04456]
1970 Jul 9.57
6.44 days
1970 Jul 16.01
Cylinder
2500?
7.5 long
2.6 dia
1970 Jul 10.3
65.44
89.23
6615
200
274
0.006
587
D
Discoverer 137
(KH 4B-24)
[Thorad 2L 556
Agena D 1654]
1970-54 A
[04477]
VDB-SLC3W
1970 Jul 23.06
26.99 days
1970 Aug 19.05
Cylinder
2000?
8 long?
1.5 dia
1970 Jul 25.2
60.00
90.04
6656
158
398
O.018
111
Intelsat 3-8
[Delta M 563 #79]
1970-55 A
[04478]
CC-LC17A
1970 Jul 23.97
1 million
years
Cylinder
137 empty
1.04 long
1.42 dia
1970 Jul 24.0
1970 Aug 1.0
2002 Dec 13.79
27.98
13.3
11.79
642.7
1043
1408.13
2466
34090
41615
282
19400
33886
36294
36030
36588
0.730
0.244
0.032
189
- *
56
Intelsat 3-8
Star-37D PKM
1970-55 B
[04486]
1970 Jul 23.97
100 years
Sphere-cone
66
1.32 long
0.94 dia
1970 Aug 6.6
2002 Dec 16.10
27.98
27.95
642.7
298.87
24666
14808
282
281
36294
16578
0.730
0.550
189
232
*
Approximate orbit, (satellite lost).
2014 – version 1.13
RAE Table of Earth Satellites
Year of Launch 1970
Name
[Launcher]
Fragments
Cospar ID
Launchdate
[Norad #] Launchsite Lifetime + Descent date
Cospar ID
[Norad]
Shape and
weight (kg)
Descent date
Size
(m)
Lifetime
Date of
orbital
determination
Orbital
Inclination
(deg)
(Revised 2002)
Nodal
period
(min)
Semi
major axis
(km)
Page 231
Perigee
height
(km)
Apogee
height
(km)
Orbital
Argument
eccentricity of perigee
(deg)
D Cosmos 354
R? [R-36-0]
1970-56 A
[04481]
BAI
1970 Jul 28.92
0.06 day
1970 Jul 28.98
Cylinder
2 long?
1 dia?
Orbit similar to
1970-56 C.
D
Cosmos 354
2nd stage
1970-56 B
[04480]
1970 Jul 28.92
0.36 day
1970 Jul 29.28
Cylinder
1500?
8 long?
2.5 dia?
1970 Jul 29.2
49.57
87.13
6514
114
157
0.003
159
D
Cosmos 354
launch platform
1970-56 C
[04479]
1970 Jul 28.92
0.49 day
1970 Jul 29.41
Irregular
-
1970 Jul 29.2
49.62
87.54
6534
134
178
0.003
58
D
Intercosmos 3
[Kosmos 11K63]
1970-57 A
[04482]
KY-LC86/4
1970 Aug 7.13
121.31 days
1970 Dec 6.44
Ellipsoid
400?
1.8 long
1.2 dia
1970 Aug 9.3
48.41
99.70
7126
200
1295
0.077
110
D
Intercosmos 3
2nd stage
1970-57 B
[04483]
1970 Aug 7.13
102.57 days
1970 Nov 17.70
Cylinder
1500?
8 long
1.65 dia
1970 Aug 9.7
48.40
99.61
7122
201
1287
0.076
112
D
R
Cosmos 355
[Voskhod 11A57]
1970-58 A
[04484]
PLE
1970 Aug 7.40
7.78 days
1970 Aug 15.18
Spherecylinder
5530?
5 long?
2.4 dia
1970 Aug 8.4
65.40
89.71
6639
199
322
0.009
45
D
Cosmos 355
Block I 3rd stage
1970-58 B
[04485]
1970 Aug 7.40
6.95 days
1970 Aug 14.35
Cylinder
2500?
7.5 long
2.6 dia
1970 Aug 9.1
65.39
89.45
6626
191
304
0.008
35
D
Cosmos 356*
[Kosmos 11K63]
1970-59 A
[04487]
PLE
1970 Aug 10.84
53.11 days
1970 Oct 2.95
Ellipsoid
400?
1.8 long
1.2 dia
1970 Aug 11.3
81.96
92.62
6780
231
573
0.025
80
D
Cosmos 356
2nd stage
1970-59 B
[04488]
1970 Aug 10.84
52.00 days
1970 Oct 1.84
Cylinder
1500?
8 long
1.65 dia
1970 Aug 11.4
81.96
92.49
6773
236
554
O.023
79
*
Atmospheric and auroral studies.
2014 – version 1.13
RAE Table of Earth Satellites
Year of Launch 1970
Name
[Launcher]
Fragments
Cospar ID
Launchdate
[Norad #] Launchsite Lifetime + Descent date
Cospar ID
[Norad]
Shape and
weight (kg)
Descent date
Size
(m)
Lifetime
Date of
orbital
determination
Orbital
Inclination
(deg)
(Revised 2002)
Nodal
period
(min)
Semi
major axis
(km)
Perigee
height
(km)
Page 232
Apogee
height
(km)
Orbital
Argument
eccentricity of perigee
(deg)
D
Venus 7 (capsule)
[Molniya 8K78M]
1970-60 A
[04489]
BAI
1970 Aug 17.23
120.00 days
1970 Dec 15.23
Sphere
455
1.0 dia
Earth->Venus
2?
287 days
0.69
1.01
0.19
Softlanded on Venus 1970 Dec 15 at 05:34:10 at 5S, 351 longitude.
Parachute descent took 32m; surface transmissions lasted 23m.
D
Venus 7
Block I 3rd stage
1970-60 B
[04490]
1970 Aug 17.23
1.17 days
1970 Aug 18.40
Cylinder
2500?
7.5 long
2.6 dia
1970 Aug 17.5
51.75
88.28
6570
182
202
0.002
280
D
Venus 7
4th stage casing
1970-60 C
[04491]
1970 Aug 17.23
1.68 days
1970 Aug 18.91
Irregular
-
1970 Aug 17.4
51.70
88.51
6582
174
233
0.004
349
Venus 7
Rocket
1970-60 D
[NNA]
1970 Aug 17.23
Cylinder
440
2.0 long
2.0 dia
Orbit unknown
D
Venus 7
(compartment)
1970-60 E
[NNA]
1970 Aug 17.23
119.98 days
1970 Dec 15.21
Cylinder +
2 vanes
725
2.5 long
1.22 dia
Earth->Venus
2?
287 days
0.69
1.01
Decayed in Venus atmosphere on 1970 Dec 15 at 05:02.
1970-60 E separeted from 1970-60 A 1970 Dec 15?
0.19
D
KH 8-28
[Tltan 3B-28
Agena D]
1970-61 A
[04492]
VDB-SLC4W
1970 Aug 18.62
16 days
1970 Sep 3
Cylinder
3000?
8 long?
1.5 dia
1970 Aug 21.2
1970 Aug 25.0
Skynet 1
[Delta M 561 #80]
1970-62 A
[04493]
CC-LC17A
1970 Aug 19.51
uncertain
Cylinder
243 full
129 empty
0.81 long
1.37 dia
Skynet 1B
Star-37D PKM
1970-62 B
[NNA]
1970 Aug 19.51
20 years?
Sphere-cone
66
D
Cosmos 357
[Kosmos 11K63]
1970-53 A
[04495]
PLE-LC133/1
1970 Aug 19.63
97.30 days
1970 Nov 24.93
D
Cosmos 357
2nd stage
1970-53 B
[04496]
D
Cosmos 358
[Kosmos 11K65M]
D
Cosmos 358
2nd stage
D
*
Fragment
1970-64 C
[04514]
Transfer orbit: present orbit unknown.
2014 – version 1.13
110.95
110.98
89.67
90.49
6636
6676
151
152
365
444
0.016
0.022
124
123
1970 Aug 20.2
28.04
636.5
24534
No current elements available at OIG
270
36041
0.729
181*
1.32 long
0.94 dia
1970 Aug 20.2
28.04
636.5
24534
270
36041
0.729
181
Ellipsoid
400?
1.8 long
1.2 dia
1970 Aug 21.1
70.99
92.04
6752
272
476
0.015
73
1970 Aug 19.63
57 days
1970 Oct 15
Cylinder
l500?
8 long
1.65 dia
1970 Aug 22.0
70.98
91.81
6741
275
450
0.013
70
1970-64 A
[04497]
PLE-LC132
1970 Aug 20.61
7250 days
1990 Jun 26
Cylinder
+ paddles?
900?
2 long?
1 dia?
1970 Aug 27.3
74.04
95.19
6905
515
539
0.002
316
1970-64 B
[04498]
1970 Aug 20.61
3243 days
1979 Jul 7
Cylinder
22OO?
7.4 long
2.4 dia
1970 Aug 24.2
1973 Oct 1.0
74.03
74.03
95.08
94.40
6900
6867
505
471
539
507
0.003
0.003
325
-
1970 Oct 29
70 days
RAE Table of Earth Satellites
Year of Launch 1970
Name
[Launcher]
Fragments
Cospar ID
Launchdate
[Norad #] Launchsite Lifetime + Descent date
Cospar ID
[Norad]
(Revised 2002)
Shape and
weight (kg)
Descent date
Size
(m)
Lifetime
Date of
orbital
determination
Orbital
Inclination
(deg)
Nodal
period
(min)
Semi
major axis
(km)
Page 233
Perigee
height
(km)
Apogee
height
(km)
Orbital
Argument
eccentricity of perigee
(deg)
D
Cosmos 359*
[Molniya 8K78M]
1970-65 A
[04501]
BAI-LC31
1970 Aug 22.22
76.04 days
1970 Nov 6.26
Spherecylinder
1180
3.5 long
1.2 dia
1970 Aug 24.3
51.13
95.57
6927
208
990
0.049
60
D
Comos 359
4th stage casing
1970-65 B
[04502]
1970 Aug 22.22
7.06 days
1970 Aug 29.28
Cylinder
2500?
7.5 long
2.6 dla
1970 Aug 23.5
51.80
89.49
6631
207
298
0.007
37
D
Cosmos 359
Block L 4th stage
1970-65 C
[04504]
1970 Aug 22.22
19 days
1970 Sep 11
D
Cosmos 359
Block I 3rd stage
1970-65 D
[04505]
1970 Aug 22.22
410 days
1971 Oct 6
Cylinder
2400**
2.0 long
2.0 dia
1970 Sep 1.0
1971 Feb 1.0
1971 Jun 1.0
51.13
51.13
51.13
95.31
93.58
91.92
6914
6830
6749
205
202
195
867
701
546
0.048
0.037
0.026
79
288
-
D
Cosmos 359
1970-65 E
SL-06 ullage motor [04506]
1970 Aug 22.22
17 days
1970 Sep 9
D
Ferret 22
[Thorad 2L 535
Agena D 2736]
1970-66 A
[04503]
VDB-SLC1W
1970 Aug 26.42
1673 days
1975 Mar 26
Cylinder
2000?
8 long?
1.5 dia
1970 Aug 29.3
1972 Apr 1.0
1974 Feb 15.0
74.99
74.99
74.99
94.51
93.87
92.57
6872
6841
6778
484
457
398
504
469
402
0.001
0.001
0.0003
256
-
Navy Navigation
Satellite 19
[Scout A S176C]
1970-67 A
[04507]
VDB-SLC5
1970 Aug 27.56
1300 years
Octagon +
4 vanes +
boom 58?
0.25 long
0.46 dia
1970 Aug 29.2
2002 Dec 15.98
90.02
89.96
107.04
106.67
7466
7451
955
943
1221
1203
0.018
0.017
245
111
Scout 4th stage
1970-67 B
[04515]
1970 Aug 27.56
700 years
Cylinder
24
1.5 long
0.46 dia
1970 Sep 6.9
2002 Dec 22.51
90.04
89.96
107.05
106.77
7467
7456
952
946
1225
1209
0.018
0.018
218
125
Fragments
1970-67 C-F
4 pieces, 1 has decayed
D
R
Cosmos 360
[Voskhod 11A57]
1970-68 A
[04508]
BAI
1970 Aug 29.36
9.93 days
1970 Sep 8.29
Spherecylinder
6300?
6.5 long
2.4 dia
1970 Sep 2.8
64.99
89.64
6635
209
305
0.007
37
D
Cosmos 360
l970-68 B
Block I 3rd stage [04509]
1970 Aug 29.36
4.34 days
1970 Sep 2.70
Cylinder
2500?
7.5 long
2.6 die
1970 Aug 31.1
65.00
88.91
6600
187
256
0.005
26
D
Cosmos 360
motor ***
1.5 long?
2 dia?
1970 Sep 7.7
64.93
88.61
6585
193
220
0.002
85
1970 Aug 29.36
Cone
11 days
600? full
1970 Sep 9
D Fragment
1970-68 D
[04517]
1970 Sep 11
D Fragment
1970-68 E
[04526]
1970 Sep 11
* Cosmos 359 was probably an attempted Venus probe.
** Mass before
***1970-68 C ejected from 1970-68 A about 1970 Sep 7.4.
2014 – version 1.13
1970-68 C
[04516]
For orbital information see extra pages at the end of the year
13 days
13 days
incomplete burn was approximately 5400kg.
RAE Table of Earth Satellites
Year of Launch 1970
Name
[Launcher]
Fragments
Cospar ID
Launchdate
[Norad #] Launchsite Lifetime + Descent date
Cospar ID
[Norad]
Shape and
weight (kg)
Descent date
Size
(m)
Lifetime
Date of
orbital
determination
Orbital
Inclination
(deg)
(Revised 2002)
Nodal
period
(min)
Semi
major axis
(km)
Perigee
height
(km)
Page 234
Apogee
height
(km)
Orbital
Argument
eccentricity of perigee
(deg)
BMEWS 4(APF 949-3) 1970-69 A
(Canyon 3)
[04510]
[Atlas SLV-3A
CC-LC13
5203A Agena D 2803]
1970 sap 1.04
> million
Cylinder
700 fu11?
years
1. 7 long?
1.4 dia?
350 empty?
1970 Sep 1.0
28.50
88.03
1970 Oct 1.0
10.3
1441.9
No elements available at OIG; orbits
2010 Feb 10.45
18.40
1436.17
2010 Apr 5.30
18.35
1436.10
Agena D rocket
l970-69 B
[27787]
1970 Sep 1.04
20 years?
Cylinder
700?
6 long?
1.5 dia
Orbit similar to 1970-46 B
DMSP B5A-02
[Thor Burner 2
# 288]
1970-70 A
[04512]
VDB-SLC10W
1970 Sep 3.36
80 years
12-faced
frustum
195
1.64 long
1.31 to
1.10 dia
1970 Sep 4.9
2002 Dec 15.84
98.73
98.83
101.30
100.50
7197
7161
764
735
874
830
0.008
0.007
21
47
Burner 2 stage
1970-70 B
[04513]
1970 Sep 3.36
60 years
Spherecone
66
1.32 long
0.94 dia
1970 Sep 9.2
2002 Dec 15.91
98.75
98.89
101.29
100.60
7197
7165
765
737
872
837
0.007
0.007
7
110
D
R
Cosmos 361
[Voskhod 11A57]
1970-71 A
[04524]
PLE
1970 Sep 8.44
12.8 days
1970 Sep 21.2
Spherecylinder
630o?
6.5 long?
2.4 dia
1970 Sep 9.1
1970 Sep 13.2
72.87
72.87
89.59
90.09
6632
6656
209
2C3
298
353
0.007
0.011
56
37
D
Cosmos 361
Block E 3rd stage
1970-71 B
[04525]
1970 Sep 8.44
5.57 days
1970 Sep 14.01
Cylinder
2500?
7.5 long
2.6 dia
1970 Sep 8.7
72.85
89.47
6626
204
291
0.007
54
D
Cosmos 361
motor*
1970-71 C
[04545]
1970 Sep 8.44
27 days
1970 Oct 5
Cone
600? full
1.5 long?
2 dia?
1970 Sep 20.2
72.87
89.95
6650
209
334
0.009
25
D
Fragment
1970-71 D
[04546]
1970 Sep 26
18 days
*
1970-71 C ejected from 1970-71 A about 1970 9ep 20.2.
2014 – version 1.13
6563
179
l90
0.001
242
42279 31947 39855 0.094
from amateur visual observations
42166 32092 39483 0.088
235
42165 32096 39477 0.088
236
RAE Table of Earth Satellites
Year of Launch 1970
Name
[Launcher]
Fragments
Cospar ID
Launchdate
[Norad #] Launchsite Lifetime + Descent date
Cospar ID
[Norad]
(Revised 2002)
Shape and
weight (kg)
Descent date
Size
(m)
Lifetime
Date of
orbital
determination
Orbital
Inclination
(deg)
Nodal
period
(min)
Semi
major axis
(km)
Page 235
Perigee
height
(km)
Apogee
height
(km)
Orbital
Argument
eccentricity of perigee
(deg)
D
R
Luna 16 #
(AS + DS)
[Proton 8K82K
240-01 / 11S824]
1970-72 A
[04527]
BAI-LC81L
1970 Sep 12.56
7.66 days
1970 sep 20.22
Pyramid + Cyl
5600?
(incl. fuel)
3.1 high
3.2 wide
3.3 deep
1970 Sep 17
1970 Sep 20.21
70
71
119
114
1848
1798
110
15
110
106
0
0.025
-$
-$
D
Luna 16
third stage
1970-72 B
[04528]
1970 Sep l2.56
3.19 days
1970 Sep 15.75
Cylinder
6.5 long?
4 dia
1970 Sep 12.9
51.53
88.70
6591
185
241
0.004
344
D
Luna 16
4th stage casing
1970-72 C
[04529]
1970 Sep 12.56
3.29 days
1970 Sep 15.85
1970 Sep 12.9
51.50
88.71
6592
186
241
0.004
334
D
Luna 16 ##
Ascent stage
1970-72 D
[NNA]
1970 Sep 12.56
11.67 days
1970 Sep 24.23
Cyl+3 spheres
800?
(incl. fuel)
2.3 high
1.6 wide
0.5 deep
Reached moon escape velocity.
D
Cosmos 362
[Kosmos 11K63]
1970-73 A
[04536]
PLE-LC133/1
1970 Sep 16.50
392.40 days
1971 Oct 13.90
Ellipsoid
400?
1.8 long
1.2 dia
1970 Sep 18.0
1971 Apr 1.0
70.96
70.96
95.65
93.26
6928
6812
270
255
829
613
0.040
0.026
82
-
D
Cosmos 362
2nd stage
1970-73 B
[04537]
1970 Sep 16.50
193.33 days
1971 Mar 28.83
Cylinder
1500?
8 long
1.65 dia
1970 Sap 17.0
1971 Jan 1.0
70.96
70.96
95.51
93.27
6921
6813
271
252
815
617
0.039
0.027
83
252
D
R
Cosmos 363
[Voskhod 11A57]
1970-74 A
[04538]
BAI
1970 Sep 17.35
11.86 days
1970 Sep 29.21
Spherecylinder
5700?
5.0 long
2.4 dia
1970 Sep 18.1
65.0l
89.53
6629
208
294
0.007
62
D
Cosmos 363
1970-74 B
Block I 3rd stage [04539]
1970 Sep 17.35
5.44 days
1970 Sep 22.79
Cylinder
2500?
7.5 1ong
2.6 dia
1970 Sep 18.1
65.00
89.33
6619
205
277
0.006
54
D
R
Cosmos 364
[Voskhod 11A57]
1970-75 A
[04553]
PLE
1970 Sep 22.54
9.76 days
1970 Oct 2.30
Spherecylinder
6300?
6.5 long?
2.4 dia
1970 Sep 25.7
1970 Oct 1.5
65.41
65.43
89.49
89.50
6628
6628
202
196
297
304
0.007
0.008
75
52
D
Cosmos 364
1970-75 B
Block I 3rd stage [04554]
1970 Sep 22.54
5.96 days
1970 Sep 28.50
Cylinder
2500?
7.5 long
2.6 dia
1970 Sep 23.2
65.40
89.5
6628
204
296
0.007
59
D
Cosmos 364
motor*
1971 Sep 22.54
17 days
1970 Oct 9
Cone
600? full
1.5 long?
2 dia?
1970 Oct 5.2
65.39
91.16
6710
222
442
0.016
2
1970-75 C
[04563]
# Orbited moon 41 times? Soft-landed 1970 Sep 20 at 05:18 at 0.68S, 56.60E. AS attached to DS till 1970 Sep 21.32
## AS relaunched 1970 Sep 21.32 from moon and landed on earth 1970 Sep 24 at 05:26 with moonsoil.
1970-75 C ejected from 1970-75 A about 1970 Oct 1.5.
2014 – version 1.13
$ Moon orbit
RAE Table of Earth Satellites
Year of Launch 1970
Name
[Launcher]
Fragments
Cospar ID
Launchdate
[Norad #] Launchsite Lifetime + Descent date
Cospar ID
[Norad]
Shape and
weight (kg)
Descent date
Size
(m)
Lifetime
Date of
orbital
determination
Orbital
Inclination
(deg)
(Revised 2002)
Nodal
period
(min)
Semi
major axis
(km)
Page 236
Perigee
height
(km)
Apogee
height
(km)
Orbital
Argument
eccentricity of perigee
(deg)
D
Cosmos 365
[R-36-0]
1970-76 A
[04556]
BAI
1970 Sep 25.59
0.06 day
1970 Sep 25.65
Cylinder
2 long?
1 dia?
Orbit similar to 1970-76 B
D
Cosmos 365
1aunch platform
1970-76 B
[04557]
1970 Sep 25.59
0.43 day
1970 Sep 26.c2
Irregular
-
1970 Sep 25.9
49.66
87.49
6532
133
114
0.003
174
D
Cosmos 365
2nd stage
1970-76 C
[04558]
1970 Sep 25.59
0.3 day?
1970 Sep 25
Cylinder
1500?
8 long?
2.5 dia?
197O Sep 25.7
49.66
87.20
6517
117
161
O.O03
-
D
Molniya-1 15
[Molniya 8K78M]
1970-77 A
[04569]
PLE
1970 Sep 29.35
1999 days
1976 Mar 20
Windmill +
6 vanes
1000?
3.4 1ong
1.6 dia
1970 Oct 1.0
1970 Nov 1.0
1971 Sep 16.0
65.5
65.3
65.75
706.18
717.57
717.63
26268
26551
26553
480
723
400
39300
39623
39949
0.739
0.733
0.745
285
284
-
D
Molniya-1 15
4th stage casing
1970-77 B
[04559]
1970 Sep 29.35
16.77 days
1970 Oct 16.12
Cylinder
2500?
7.5
2.6
1970 Oct 1.6
65.39
90.99
6702
205
443
0.018
57
D
Molniya-1 15
1970-77 C
Block I 3rd stage [04560]
1970 Sep 29.35
24.08 days
1970 Oct 23.43
Irregular
-
1970 Sep 30.9
65.43
91.50
6727
228
469
0.018
74
D
Molniya-1 15
1970-77 D
Block L 4th stage [04570]
1970 sep 29.35
610 days
1972 May 31
Cylinder
440
2.0
2.0
1970 Nov 1.0
1971 Apr 1.0
1971 Sep 1.0
65.41
65.6
65.8
704.67
704.43
704.07
26231
26225
26216
490
358
236
39215
39335
39439
0.738
0.743
0.748
-
D
Fragment
1970-77 E
[05950]
1972 Apr 30
579 days
D
R
Cosmos 366
[Voskhod 11A57]
1970-78 A
[04561]
BAI
1970 Oct 1.35
11.9 days
1970 Oct 13.3
Spherecylinder
5700?
5.0
2.4
long
dia
1970 Oct 2.5
64.96
89.48
6628
204
295
0.007
39
D
Cosmos 366
1970-78 B
Block I 3rd stage [04562]
1970 Oct 1.35
5 days
1970 Oct 6
Cy1inder
2500?
7.5
2.6
long
dia
1970 Oct 3.1
64.96
89.13
6610
177
286
0.008
42
2014 – version 1.13
long
dia
long
dia
RAE Table of Earth Satellites
Year of Launch 1970
Name
[Launcher]
Fragments
Cospar ID
Launchdate
[Norad #] Launchsite Lifetime + Descent date
Cospar ID
[Norad]
(Revised 2002)
Shape and
weight (kg)
Descent date
Size
(m)
Lifetime
Date of
orbital
determination
Orbital
Inclination
(deg)
Nodal
period
(min)
Semi
major axis
(km)
Page 237
Perigee
height
(km)
Apogee
height
(km)
Orbital
Argument
eccentricity of perigee
(deg)
Cosmos 367#
[Tsyklon 2]
1970-79 A
[04564]
BAI-LC90
1970 Oct 3.44
600 years
Conecylinder
6 long?
2 dia?
1970 Oct 6.8
2002 Dec 17.83
65.23
65.28
104.53
104.47
7351
7348
922
931
1024
1009
0.007
0.005
312
136
D
Cosmos 367
2nd stage
1970-79 B
[04565]
1970 Oct 3.44
2.93 days
1970 Oct 6.37
Cylinder
1500?
8 long?
2.5 dia?
1970 Oct 4.9
65.21
89.21
6614
226
246
0.002
227
D
Cosmos 367
platform
1970-79 C
[04566]
1970 Oct 3.44
27.69 days
1970 Oct 31.13
Irregular
-
1970 Oct 4.8
65.09
89.60
6633
246
264
0.001
258
D
D
Fragment
Fragment
1970-79 D
1970-79 E
[04567]
[04568]
1970 Oct 8
1970 Oct 12
5 days
9 days
D
B
R
Cosmos 368/Bion 1
[Voskhod 11A57]
1970-80 A
[04571]
BAI
1970 Oct 8.53
5.98 days
1970 Oct 14.51
Spherecylinder
5900?
5.9 long
2.4 dia
1970 Oct 9.7
64.99
90.56
6680
204
400
0.015
56
D
Cosmos 368
1970-80 B
Block I 3rd stage [04572]
1970 Oct 8.53
11.60 days
1970 Oct 20.13
Cylinder
25O0?
7.5 long
2.6 dia
1970 Oct 9.7
65.00
90.43
6674
203
389
0.014
52
D
Cosmos 368 *
Capsule/Pickaback
1970-80 E
[04585]
1970 Oct 8.53
27 days
1970 Nov 4
Ellipsoid
200?
0.9 long
1.9 dia
1970 Nov 1.0
64.9
88.70
6589
178
243
0.005
-
D
D
Fragment
Fragment
1970-80 C
1970-80 D
[04575]
[04582]
1971 Jan 7
1970 Oct 19
91 days
11 days
D
Cosmos 369
[Kosmos 11K63]
1970-81 A
[04573]
PLE-LC133/1
1970 Oct 8.63
106.20 days
1971 Jan 22.83
Ellipsoid
400?
1.8 long
1.2 dia
1970 Oct 9.6
70.93
92.32
6766
269
506
0.018
86
D
Cosmos 369
ro&et
1970-81 B
[04574]
1970 Oct 8.63
52.76 days
1970 Nov 30.39
Cylinder
1500?
8 long
1.65 dia
1970 Oct 10.9
70.93
92.15
6757
271
486
0.016
84
*
#
1970 ejected from 1970-80 A m 1970 Oct 13
1970-79 B and 79 C attached to 1970-79 A until orbit change. First operational Rorsat.
2014 – version 1.13
RAE Table of Earth Satellites
Year of Launch 1970
Name
[Launcher]
Fragments
Cospar ID
Launchdate
[Norad #] Launchsite Lifetime + Descent date
Cospar ID
[Norad]
(Revised 2002)
Shape and
weight (kg)
Descent date
Size
(m)
Lifetime
Date of
orbital
determination
Orbital
Inclination
(deg)
Nodal
period
(min)
Semi
major axis
(km)
Page 238
Perigee
height
(km)
Apogee
height
(km)
Orbital
Argument
eccentricity of perigee
(deg)
D
R
Cosmos 370
[Voskhod 11A57]
1970-82 A
[04576]
BAI
1970 Oct 9.46
12.84 days
1970 Oct 22.30
3pherecylinder
6300?
6.5 long?
2.4 dia
1970 Oct 10.9
64.92
89.40
6623
202
288
0.006
33
D
Cosmos 370
1970-82 B
Block I 3rd stage [04577]
1970 Oct 9.46
4.13 days
1970 Oct 13.59
Cylinder
2500?
7.5 long
2.6 dia
1970 Oct 11.7
64.93
88.77
6392
187
241
0.004
9
D
Cosmos 370
motor*
1970-82 C
[04593]
1970 Oct 9.46
18 days
1970 Oct 27
Cone
60O? full
1.5 long?
2 dia?
1970 Oct 22.3
64.92
88.74
6591
182
243
0.005
-
Cosmos 371
[Kosmos 11k65M]
1970-83 A
[04578]
PLE-LC132
1970 Oct 12.58
100 years
Cylinder +
paddles?
750?
2 long?
1 dia?
1970 Oct 31.0
2002 Dec 18.14
74.00
74.00
99.92
99.17
7132
7097
750
717
758
720
0.0005
0.0002
16
122
Cosmos 371
2nd stage
1970-83 B
[04579]
1970 Oct 12.58
80 years
Cylinder
2200?
7.4 long
2.4 dia
1970 Oct 12.9
2002 Dec19.85
74.00
74.00
99.81
98.78
7127
7079
743
692
755
709
0.0009
0.001
107
335
D
Intercosmos 4
[Kosmos 11K63]
1970-84 A
[04580]
KY-LC86/4
1970 Oct 14.48
95.20 days
1971 Jan 17.68
Ellipsoid +
6 panels
400?
1.13 long
1.2 dia
1970 Oct 16.9
48.41
93.56
6830
255
649
0.029
l18
D
Intercosmos 4
2nd stage
1970-84 B
[04581]
1970 Oct 14.48
63.63 days
1970 Dec 17.11
Cylinder
1500?
8 long
1.65 dia
1970 Oct 16.7
48.41
93.29
6817
259
619
0.026
117
D
Meteor-1 6
[Vostok 8A92M]
1970-85 A
[04583]
PLE
1970 Oct 15.48
10312 days
1999 Jan 8.3
Cylinder +
2 vanes
220O?
5 long?
1.5 dia?
1970 Oct 25.1
81.21
97.49
7015
626
648
0.002
56
D
Meteor-1 6
rocket
1970-85 B
[04584]
1970 Oct 15.48
11036.03 days
2001 Jan 1.51
Cylinder
1440
3.8 long
2.6 dia
1970 Oct 22.3
81.23
97.62
7022
551
736
0.013
155
D
Fragment
1970-85 C
[06330]
1990 Mar 10
7086 days
*1970-82 C ejected from 1970-82 A on 1970 Oct 21 or 22.
2014 – version 1.13
RAE Table of Earth Satellites
Year of Launch 1970
Name
[Launcher]
Fragments
Cospar ID
Launchdate
[Norad #] Launchsite Lifetime + Descent date
Cospar ID
[Norad]
(Revised 2002)
Shape and
weight (kg)
Descent date
Size
(m)
Lifetime
Date of
orbital
determination
Orbital
Inclination
(deg)
Nodal
period
(min)
Semi
major axis
(km)
Page 239
Perigee
height
(km)
Apogee
height
(km)
Orbital
Argument
eccentricity of perigee
(deg)
Cosmos 372
[Kosmos 11K65M
53717-04]
1970-86 A
[04588]
PLE-LC132
1970 Oct 16.63
100 years
Cylinder +
paddles?
750?
2 1ong?
1 dia?
1970 Oct 29.2
2002 Dec 17.86
74.06
74.05
100.80
100.33
7174
7153
735
765
806
785
0.001
0.001
9
209
Cosmos 372
2nd stage
1970-86B
[04589]
1970 Oct 16.63
80 years
Cylinder
220O?
7.4 long
2.4 dia
1970 Oct 29.2
2002 Dec 19.56
74.06
74.06
100.70
100.02
7169
7138
776
745
806
774
0.002
0.002
7
126
D
Fragment
Fragment
1970-86 C
1970-86 D
[05357]
[05358]
2004 Apr 2
12222 days
2002 Dec 16.43
2002 Dec 15.45
74.01
74.04
94.93
97.78
6894
7031
515
650
516
656
0.0001
0.0005
285
28
D
Cosmos 373
[Tsyklon 2]
1970-87 A
[04590]
BAI-LC90
1970 Oct 20.24
3427 days
1980 Mar 8
Cylinder?
4 long?
2 dia?
1970 Oct 20.5
1970 Oct 31.1
62.93
62.92
94.77
94.83
6886
6889
472
466
544
556
0.005
0.006
290
311
D
Cosmos 373
r~t
1970-87 B
[04595]
1970 Oct 20.24
90 days
1971 Jan 18
Cylinder
1500?
8 long?
2.5 dia?
1970 Oct 23.2
62.26
95.45
6919
145
937
0.057
54
D
R
Zond 8 (capsule)
[Proton8K82K
250-01 / 11S824]
1970-88 A
[04591]
BAI-LC81L
1970 Oct 20.83
6.75 days
1970 Oct 27.58
Spheroid
2760?
2.2 dia
Passed 1120 km beyond moon 1970 Oct 24.1
Landed on Earth 1970 Oct 27 at 13:55.
D
Zcnd 8
third stage
1970-88 B
[04592]
1970 Oct 20.83
6 days
1970 Oct 26
Cylinder
6.5 long?
4 dia
1970 Oct 21.6
202
223
0.002
338
Zond 8
4th stage
1970-88 C
[NNA]
1970 Oct 20.83
Cylinder
1900?
3.9 long?
3.9 dia
Orbit unknown
Zond 8
Compartment
1970-88 D
[NNA]
1970 Oct 20.83
6.74 days
1970 Oct 27.57
Cylinder +
2 paddles
2615?
3.1 long
2.3 dia
Attached to Zond * capsule until decay in Earth's atmosphere
1970 Oct 27 at 13:41.
Cosmos 374*
[Tsyklon 2]
1970-89 A
[04594]
BAI-LC90
1970 Oct 23.18
150 years
Cylinder?
4 long?
2 dia?
1970 Oct 30.2
2002 Dec 15.87
62.95
62.95
112.26
104.80
7709
7364
521
516
2141
1455
0.105
0.064
61
19
Cosmos 374
2nd stage
1970-89 B
[04597]
1970 Oct 23.18
100 years
Cylinder
1500?
8 long?
2.5 dia?
1970 Oct 28.5
2002 Dec 20.78
62.93
62.94
111.83
111.32
7690
7666
517
541
2106
2034
0.103
0.097
62
18
Fragments
1970-89 C-DG
D
KH 8-29
[Titan 3B-29
Agena D]
197O-90 A
[04596]
VDB-SLC4W
*
1970-89 A passed close to 1970-87 A on Oct 23.34, then exploded.
D
2014 – version 1.13
101 pieces, 80 have decayed
1970 Oct 23.74
19 days
1970 Nov 11
Cylinder
3000?
51.51
88.68
6591
For orbital information see extra pages at the end of the year
8 long?
1.5 dia
1970 Oct 24.3
1ll.06
89.83
6644
135
396
0.020
137
RAE Table of Earth Satellites
Year of Launch 1970
Name
[Launcher]
Fragments
Cospar ID
Launchdate
[Norad #] Launchsite Lifetime + Descent date
Cospar ID
[Norad]
(Revised 2002)
Shape and
weight (kg)
Descent date
Size
(m)
Lifetime
Date of
orbital
determination
Orbital
Inclination
(deg)
Nodal
period
(min)
Semi
major axis
(km)
Page 240
Perigee
height
(km)
Apogee
height
(km)
Orbital
Argument
eccentricity of perigee
(deg)
Cosmos 375
[Tsyklon 2]
1970-91 A
[04598]
BAI-LC90
1970 Oct 30.09
150 years
Cylinder?
4 long?
2 dia?
1970 Nov 3.0
2002 Dec 18.34
62.82
62.84
111.82
111.85
7689
7660
524
576
2098
1987
0.102
0.092
56
294
Cosmos 375
rocket
1970-91 B
[04622]
1970 Oct 30.09
11631 days
2002 Sep 3
Cylinder
1500?
8 long?
2.5 dia?
1970 Nov 3.9
62.78
111.52
7674
526
2066
0.100
56
Fragments
1970-91 C-AY 45 pieces, 21 have decayed
D
R
Cosmos 376
[Voskhod 11A57]
l970-92 A
[04599]
PLE
1970 Oct 30.56
12.71 days
1970 Nov 12.27
Spherecylinder
6300?
6.5 long?
2.4 dia
1970 Oct 31.9
1970 Nov 10.3
65.38
65.42
89.43
89.23
6625
6616
207
203
286
272
0.006
0.005
73
65
D
Cosmos 376
Block I 3rd stage
1970-92 B
[04600]
1970 Oct 30.56
5.61 days
1970 Nov 5.17
Cylinder
2500?
7.5 long
2.6 dia
1970 Oct 31.8
65.40
89.22
6614
209
263
0.004
62
D
Cosmos 376
motor**
1970-92 C
[04700]
1970 Oct 30.56
21 days
1970 Nov 20
Cone
600? full
1.5 long?
2 dia?
1970 Nov 15.6
65.36
88.67
6588
192
228
0.003
70
IMEWS 1 #
[Titan 3C 23C-1]
1970-93 A
[04630]
CC-LC40
1970 Nov 6.44
>million
years
cylinder
+ 4 panels
820?
6 long?
2.5 dia?
1970 Nov 7.1
1970 Dec 1.0
2002 Dec 13.16
26.29
7.8
12.42
635.1
1197.1
1197.83
24473
37346
37361
300
26050
25617
35890
35886
36349
0.727
0.132
0.144
180
189
IMEWS 1
Transtage 19
1970-93 B
04632]
1970 Nov 6.44
> million
years
Cylinder
1500?
6 long?
3 dia
Orbit similar to
2002 Dec 12.93
1970-93 A
12.39
1197.68
37358
25579
36380
0.145
189
Titan 3C
second stage
1970-93 C
[04631]
1970 Nov 6.44
1.51 days
1970 Nov 7.95
Cylinder
1900
6 long
3.0 dia
1970 Nov 7.1
28.6
6617
147
331
0.014
120
D
D
For orbital information see extra pages at the end of the year
89.15
* 1970-91 A passed close to 1970-87 A on Oct 30.25.
** Motor probably ejected about Nov 10.
# Integrated Missile Early Warning Satellite, aka DSP 01; AFP 647-01. Remained in transfer-orbit when fuel exhausted.
2014 – version 1.13
RAE Table of Earth Satellites
Year of Launch 1970
Name
[Launcher]
Fragments
Cospar ID
Launchdate
[Norad #] Launchsite Lifetime + Descent date
Cospar ID
[Norad]
1970-94 A
[04690]
WLI-LA3
(Revised 2002)
Shape and
weight (kg)
Descent date
Size
(m)
Lifetime
Date of
orbital
determination
Orbital
Inclination
(deg)
Nodal
period
(min)
Semi
major axis
(km)
1970 Nov 9.25
180.95 days
1971 May 9.21
Octagonal
cylinder
133
1.19 long
0.76 dia
1970 Nov 11.1
1971 Feb 1.0
37.41
37.41
92.64
91.86
Cylinder
45
(payload 21)
1.68 long
0.76 dia
1970 Nov 11.1
37.41
92.71
Page 241
Perigee
height
(km)
Apogee
height
(km)
Orbital
Argument
eccentricity of perigee
(deg)
6789
6750
304
278
518
466
0.016
0.014
134
-
6793
303
526
0.016
133
D
B
Orbiting Frog
Otolith 1
[Scout B S178C]
D
Radiation Meteo- 1970-94 B
roid OFO 1 rocket [04692]
1970 Nov 9.25
90.15 days
1971 Feb 7.40
D
Fragments
1970-94 C-E
3 pieces, all have decayed
D
Luna 17 **
]Proton 8K82K
251-01 / 11S824]
1970-95 A
[04691]
BAI-LC81L
1970 Nov 10.61
6.55 days
1970 Nov 17.16
Pyramid + car
5600?
(incl. fuel)
2.3 high
3.2 width
3.3 deep
1970 Nov 15
1970 Nov 17.15
141
141
116
114
1823
1790
85
19
85
85
0
0.018
-$
-$
D
Luna 17
third stage
1970-95 B
[04694]
1970 Nov 10.61
2.96 days
1970 Nov 13.57
Cylinder
6.5 long?
4 dia
1970 Nov 11.5
51.53
88.57
6584
184
228
0.003
299
D
Luna 17
4th stage casing
1970-95 C
[04697]
1970 Nov 10.61
3.00 days
1970 Nov 13.61
-
-
1970 Nov 10.8
51.55
88.73
6593
192
237
0.003
296
D
Luna 17
4th stage
1970-95 D
[NNA]
1970 Nov 10.61
Cylinder
1900?
3.9 long?
3.9 dia
Orbit unknown
D
R
Cosmos 377
[Voskhod 11A57]
1970-96 A
[04695]
BAI
1970 Nov 11.39
11.9 days
1970 Nov 23.3
Spherecylinder
5700?
5.0 long
2.4 dia
1970 Nov 11.8
64.99
89.40
6623
204
286
0.006
44
D
Cosmos 377
Block I 3rd stage
1970-96 B
[04696]
1970 Nov 11.39
5.49 days
1970 Nov 16.88
Cylinder
2500?
7.5 long
2.6 dia
1970 Nov 11.4
54.98
89.36
6621
201
285
0.006
39
D
Cosmos 378*
[Kosmos 11K65M
47117-107]
1970-97 A
[04713]
PLE-LC132/2
1970 Nov 17.77
638.86 days
1972 Aug 17.63
Octagonal
ellipsoid?
400?
1.8 long?
1..5 dia?
1970 Nov 20.0
1971 Oct 16.5
74.00
74.00
104.88
99.95
7366
7133
234
227
1742
1283
0.102
0.074
122
-
D
Cosmos 378
2nd stage
1970-97B
[04714]
1970 Nov 17.77
682.98 days
1972 Sep 30.75
Cylinder
2200?
7.4 long
2.4 dia
1970 Nov 20.0
1971 Nov 16.0
74.00
74.00
104.75
99.99
7360
7135
233
222
1730
1292
0.102
0.075
1 21
-
For orbital information see extra pages at the end of the year
* Ionospheric studies
** Inclueded Lunokhod 1, a 756 kg roving vehicle; 1.45 m high, 2.15 m wide, 2.22 m long.
Orbited moon 28 times. Soft-landed 1970 Nov 17 at 03:47 at 38.28S, 35W.
2014 – version 1.13
$ Moon orbit
RAE Table of Earth Satellites
Year of Launch 1970
Name
[Launcher]
Fragments
Cospar ID
Launchdate
[Norad #] Launchsite Lifetime + Descent date
Cospar ID
[Norad]
(Revised 2002)
Shape and
weight (kg)
Descent date
Size
(m)
Lifetime
Date of
orbital
determination
Orbital
Inclination
(deg)
Nodal
period
(min)
Semi
major axis
(km)
Page 242
Perigee
height
(km)
Apogee
height
(km)
Orbital
Argument
eccentricity of perigee
(deg)
D
Discoverer 138
(KH 4B-25)
[Thorad 2L 552
Agena D 1658]
1970-98 A
[04721]
VDB-SLC3W
1970 Nov 18.89
22.78 days
1970 Dec 11.67
Cylinder
2000?
8 long?
1.5 dia
1970 Nov 21.0
82.99
88.70
6587
185
232
0.004
164
D
Hitchhiker 28*
1970-98 B
[04722]
1970 Nov 18.89
2492 days
1977 Sep 14
Octagon?
60?
0.3 long?
0.9 dia?
1970 Nov 20.5
1972 Sep 1.0
83.18
83.18
94.63
93.95
6877
6844
487
455
511
477
0.002
0.002
258
-
D
Cosmos 379
[Soyuz 11A511L]
1970-99 A
[04760]
BAI
1970 Nov 24.22
4684 days
1983 Sep 21
-
-
1970
1970
1970
1973
24.9
25.9
30.2
1.0
51.62
51.62
51.69
51.70
88.67
98.73
259.64
225. 2
6590
7078
13483
12262
192
190
175
174
232
1210
14035
11593
0.003
0.072
0.514
0.466
80
62
72
-
D
Cosmos 379
Block I 3rd stage
1970-99 B
[04761]
1970 Nov 24.22
2.34 days
1970 Nov 26.56
Cylinder
2500?
7.5 long
2.6 dia
1970 Nov 24.9
51.61
88.46
6580
189
214
0.002
59
D
Cosmos 379
platform
1970-99 C
[04780]
1970 Nov 24.22
81 days
1971 Feb 13
-
-
1970 Nov 27.4
51.52
98.58
7071
187
1198
0.071
67
D
Fragment
1970-99 D
[04817]
1971 Jan 2
39 days
D
Cosmos 380
[Kosmos 11K63]
1970-100 A
[04762]
PLE-LC133/1
1970 Nov 24.46
205.43 days
1971 Jun 17.89
Ellipsoid
400?
1.8 long
1.2 dia
1970 Nov 25.2
1971 Mar 1.0
81.95
81.95
102.15
98.39
7238
7059
199
195
1520
1167
0.091
0.069
73
-
D
Cosmos 380
2nd stage
1970-100 B
[04763]
1970 Nov 24.46
135.76 days
1971 Apr 9.22
Cylinder
15007
8 long
1.65 di.a
1970 Nov 25.8
1971 Feb 1.0
81.96
81.96
101.93
98.40
7227
7060
197
193
1501
1170
0.090
0.069
71
-
*
1970-98 B ejected from 1970-98 A on 1970 Nov 18.96.
2014 – version 1.13
Nov
Nov
Nov
Jun
RAE Table of Earth Satellites
Year of Launch 1970
Name
[Launcher]
Fragments
Cospar ID
Launchdate
[Norad #] Launchsite Lifetime + Descent date
Cospar ID
[Norad]
(Revised 2002)
Shape and
weight (kg)
Descent date
Size
(m)
Lifetime
Date of
orbital
determination
Orbital
Inclination
(deg)
Nodal
period
(min)
Page 243
Semi
major axis
(km)
Perigee
height
(km)
Apogee
height
(km)
Orbital
Argument
eccentricity of perigee
(deg)
D
Molniya-1 16
[Molniya 8K78M]
1970-101 A
[04779]
PLE
1970 Nov 27.66
1824 days
1975 Nov 25
Windmill
6 vanes
1000?
3.4 long
1.6 dia
1970 Nov 29.2
1971 Jan 1.0
1973 Feb 1.0
65.48
65.49
65.50
707.09
717.81
717.73
26292
26557
26555
471
463
1379
39356
39895
38975
0.740
0.742
0.708
285
-
0
Molnlya-1 16
Block I 3rd stage
1970-101 B
[04781]
1970 Nov 27.66
13.69 days
1970 Dec 11.35
Cylinder
2500?
7.5 long
2.6 dia
1970 Nov 28.8
65.42
90.61
6683
213
397
0.014
'51
D
Molniya-1 16
4th stage casing
1970-101 C
[04782]
1970 Nov 27.66
20.08 days
1970 Dec 17.74
Irregular
-
1970 Nov 29.5
65.39
91.02
6703
216
434
0.016
60
D
Molniya-1 16
Block L 4th stage
1970-101 D
[04785]
1970 Nov 27.66
1862 days
1976 Jan 2
Cylinder
440
?.0 long
2.0 dia
1970 Nov 30.6
1973 Feb 1.0
65.41
65.46
707.99
702.97
26190
26190
412
1 350
39212
38273
0.741
0.705
285
-
Cosmos 381*
[Kosmos 11K65M
47117-105]
1970-102 A
[04783]
PLE-LC132
1970 Dec 2.17
1200 years
Cylinder +
boom
700?
1.4 long
2.0 dia
1970 Dec 7.6
2002 Dec 17.69
74.04
74.03
104.93
104.77
7369
7362
968
961
1013
1006
0.003
0.003
270
304
Cosmos 381
2nd stage
1970-102 B
[04784]
1970 Dec 2.17
500 years
Cylinder
2200?
7.4 long
2.4 dla
1970 Dec 4.6
2002 Dec 17.90
74.03
74.03
104.82
104.63
7364
7356
967
958
1004
997
0.002
0.003
263
249
Fragments
1970-102 C-F 4 pieces, 2 have decayed
Cosmos 382
[Proton 8K82K
252-01/11S284-26]
1970-103 A
[04786]
BAI-LC81L
1970 Dec 2.69
1000 years
Sphere?
5 dia?
1970
1970
1970
2002
4.5
7.4
8.0
20.85
51.54
51.55
55.87
55.84
142.82
158.93
171.06
171.00
9053
9722
10208
10206
305
1615
2577
2382
5045
5072
5082
5273
0.262
0.178
0.123
0.142
261
258
248
108
Cosmos 382
Third stage
1970-103 B
[04789]
1970 Dec 2.69
30O00 years
Cylinder
6.5 long?
4 dia
1970 Dec 5.1
1971 Jan 1.0
2002 Dec 15.74
51.53
51.54
51.59
144.07
158.74
158.80
9105
9714
9714
409
1590
1589
5045
5081
5082
0.255
0.180
0.180
261
285
203
Cosmos 382
platform
1970-103 C
[04790]
1970 Dec 2.69
30000 years
-
-
1970 Dec 14.4
2002 Dec 15.92
51.59
51.57
159.07
159.10
9727
9727
1614
1610
5084
5087
0.178
0.179
266
130
Fragments
1970-103 D-G 4 pieces, 3 have decayed
*
Topside Ionospheric sounder
2014 – version 1.13
For orbital information see extra pages at the end of the year
Dec
Dec
Dec
Dec
For orbital information see extra pages at the end of the year
RAE Table of Earth Satellites
Year of Launch 1970
Name
[Launcher]
Fragments
Cospar ID
Launchdate
[Norad #] Launchsite Lifetime + Descent date
Cospar ID
[Norad]
Size
(m)
Lifetime
Date of
orbital
determination
Orbital
Inclination
(deg)
Nodal
period
(min)
Semi
major axis
(km)
1970 Dec 3.58
12.69 days
1970 Dec 16.27
Spherecylinder
6300?
6.5 long?
2.4 dia
1970 Dec 4.7
1970 Dec 14.1
65.41
65.42
89.33
89.53
Page 244
Perigee
height
(km)
Apogee
height
(km)
Orbital
Argument
eccentricity of perigee
(deg)
6620
6630
204
181
279
323
0.006
0.011
57
53
D
R
Cosmos 383*
[Voskhod 11A57]
D
Cosmos 383
1970-104 B
Block I 3rd stage [04788]
1970 Dec 3.58
6.12 days
1970 Dec 9.70
Cylinder
2500?
7.5 long
2.6 dia
1970 Dec 4.4
65.40
89.15
6611
200
266
0.005
55
D
R
Cosmos 384
[Voskhod 11A57]
1970-105 A
[04791]
PLE
1970 Dec 10.47
11.80 days
1970 Dec 22.27
Spherecylinder
5900?
5.9 long
2.4 dia
1970 Dec 11.5
72.88
89.46
6626
203
292
0.007
57
D
Cosmos 384
1970-105 B
Block I 3rd stage [04792]
1970 Dec 10.47
5.31 days
1970 Dec 15.78
Cylinder
2500?
7.5 long
2.6 dia
1970 Dec 12.4
72.89
89.16
6610
195
268
0.005
41
D
Capsule
Pickaback
1970-105 E
[04810]
1970 Dec 10.4
17 days
1970 Dec 27
Ellipsoid
200?
0.9 long
1.9 dia
1970 Dec 18.3
72.88
89.27
6616
204
271
0.005
44
D
D
Fragment
Fragment
1970-105 C
1970-105 D
[04795]
[04796]
1970 Dec 18
1970 Dec 18
8 days
8 days
NOAA 1 #
1970-106 A
(ITOS)
[04793]
[Delta N6 546 #81] VDB-SLC2W
1970 Dec 11.42
10000 years
Box
306
1.25 long
1970 Dec 20.9
1.02 square 2002 Dec 17.89
101.94
101.74
114.93
114.83
7829
7826
1429
1423
1473
1473
0.003
0.003
237
305
NOAA 1
2nd stage(CEP1)##
1970-106 B
[04794]
1970 Dec 11.48
5000 years
Cylinder
350?
4.9 long
1.43 dia
1970 Dec 24.9
2002 Dec 17.95
101.92
101.82
114.91
114.90
7828
7829
1425
1422
1475
1480
0.003
0.004
226
305
Fragment
1970-106 C
[08828]
2002 Dec 16.11
102.10
116.32
7893
1489
1541
0.003
269
*
**
#
##
1970-104 A
[04787]
PLE
(Revised 2002)
Shape and
weight (kg)
Descent date
Cosmos 383 manoeuvred, but no jettisoned engine was tracked or designated.
1970-105 E ejected from 1970-105 A on 1970 Dec 17.6
National Oceanic and Atmospheric Administration
Cylindrical Electrostatic Probe
2014 – version 1.13
RAE Table of Earth Satellites
Year of Launch 1970
Name
[Launcher]
Fragments
Cospar ID
Launchdate
[Norad #] Launchsite Lifetime + Descent date
Cospar ID
[Norad]
(Revised 2002)
Shape and
weight (kg)
Descent date
Size
(m)
Lifetime
Date of
orbital
determination
Orbital
Inclination
(deg)
Nodal
period
(min)
Semi
major axis
(km)
Page 245
Perigee
height
(km)
Apogee
height
(km)
Orbital
Argument
eccentricity of perigee
(deg)
D
Explorer 42
(SAS 1, Uhuru)*
[Scout B S175C]
1970-107 A
[04797]
SMC
1970 Dec 12.45
3036 days
1979 Apr 5
Cylinder
4 paddles
143
1.16 long
0.56 dia
1970 Dec 12.7
3.04
95.30
6921
522
563
0.003
0
D
Explorer 42
Scout 4th stage
1970-107 B
[04798]
1970 Dec 12.45
2925 days
1978 Dec 15 A
Cylinder
24
1.50 long
0.46 dia
1970 Dec 12.4
2.91
95.22
6917
529
549
0.002
352
Cosmos 385
[Kosmos 11K65M
V149-39]
1970-108 A
[04799]
PLE-LC132
1970 Dec 12.54
1200 years
Cylinder +
boom?
700?
1.4 long
2.0 dia
1970 Dec 15.9
2002 Dec 18.46
74.02
74.02
104.75
104.60
7360
7354
978
973
986
979
0.0005
0.0004
312
281
Cosmos 385
2nd stage
1970-108 B
[04800]
1970 Dec 12.54
600 years
Cylinder
2200?
7.4 long
2.4 dia
1970 Dec 15.3
2002 Dec 18.36
74.02
74.02
104.64
104.47
7355
7348
974
964
979
976
0.0003
0.0009
129
3
D
Peole 1
[Diamant B #2]
1970-109 A
[04801]
KOU-ELD
1970 Dec 12.54
3474 days
1980 Jun 16
Octahedron
70
0.55 long
0.70 dia
1971 Jan 12.8
15.00
97.17
7010
517
747
0.016
248
D
Peole 1
3rd stage
1970-109 B
[04802]
1970 Dec 12.54
11334 days
2001 Dec 23
Cylinder
68
1.60 long?
0.65 dia
1970 Dec24.7
15.00
98.43
7070
635
749
0.008
319
D
D
D
D
Fragment
Fragment
Fragment
Fragment
1970-109
1970-109
1970-109
1970-109
[04803]
[04839]
[05264]
[05952]
1980
1979
1980
1976
C
D
E
F
* Small Astronomical Satellite.
** Préliminaire à Eole.
2014 – version 1.13
May
Apr
Jan
Oct
14
20 A
6 A
30
3441
3051
3312
2149
days
days
days
days
RAE Table of Earth Satellites
Year of Launch 1970
Name
[Launcher]
Fragments
Cospar ID
Launchdate
[Norad #] Launchsite Lifetime + Descent date
Cospar ID
[Norad]
(Revised 2002)
Shape and
weight (kg)
Descent date
Size
(m)
Lifetime
Date of
orbital
determination
Orbital
Inclination
(deg)
Nodal
period
(min)
Semi
major axis
(km)
Page 246
Perigee
height
(km)
Apogee
height
(km)
Orbital
Argument
eccentricity of perigee
(deg)
D
R
Cosmos 386
[Voskhod 11A57]
1970-110 A
[04804]
BAI
1970 Dec 15.42
12.9 days
1970 Dec 28.3
Spherecylinder
6300?
6.5 long?
2.4 dia
1970 Dec 16.5
64.99
89.40
6624
215
276
0.005
52
D
Cosmos 386
1970-110 B
Block I 3rd stage [04805]
1970 Dec 15.42
3.88 days
1970 Dec 19.30
Cylinder
2500?
7.5 long
2.6 dia
1970 Dec 16.2
65.01
88.91
6599
196
245
0.004
8
D
Cosmos 386
motor*
1970-110 E
[04836]
1970 Dec 15.42
19 days
1971 Jan 3
Cone
600? full
1.5 long?
2 dia?
1970 Dec 29.6
64.99
89.77
5642
213
315
0.008
40
D
D
D
Fragment
Fragment
Fragment
1970-110 C
1970-110 D
1970-110 F
[04808]
[04835]
[04838]
1970 Dec 17
1971 Jan 12
1971 Jan 2
2 days
28 days
18 days
D
Cosmos 387
[Kosmos 11K65M
V149-31]
1970-111 A
[04806]
PLE-LC132
1970 Dec 16.19
3321 days
1980 Jan 19
Cylinder
paddles?
900?
2 long?
1 dia?
1970 Dec 24.0
74.01
95.31
6911
528
538
0.0008
6
D
Cosmos 387
2nd stage
1970-111 B
[04807]
1970 Dec 16.19
3387 days
1980 Mar 25
Cylinder
2200?
7.4 long
2.4 dia
1970 Dec 24.0
74.01
95.13
6902
513
535
0.002
31
D
D
D
Fragment
Fragment
Fragment
1970-1l1 C
1970-1l1 D
1970-1l1 E
[04809]
[04815]
[04816]
1971 Dec 12
1971 Sep 3
1971 Aug 24
361 days
261 days
251 days
D
Cosmos 388
[Kosmos 11K63]
1970-112 A
[04811]
PLE-LC133/1
1970 Dec 18.40
143.40 days
1971 May 10.80
Ellipsoid
400?
1.8 long
1.2 dia
1970 Dec 20.3
1971 Mar 1.0
70.95
70.95
92.32
91.51
6766
6726
271
257
505
439
0.017
0.014
78
-
D
Cosmos 388
2nd stage
1970-112 B
[04812]
1970 Dec 18.40
61.35 days
1971 Feb 17.75
Cylinder
1500?
8 long
1.65 dia
1970 Dec 20.4
70.96
92.18
6759
268
494
0.017
79
*
1970-110 E ejected from 1970-110 A about 1970 Dec 28.
2014 – version 1.13
RAE Table of Earth Satellites
Year of Launch 1970
Name
[Launcher]
Fragments
D
Cosmos 389
[Vostok 8A92M]
Cospar ID
Launchdate
[Norad #] Launchsite Lifetime + Descent date
Cospar ID
[Norad]
(Revised 2002)
Shape and
weight (kg)
Descent date
Size
(m)
Lifetime
Date of
orbital
determination
Orbital
Inclination
(deg)
Nodal
period
(min)
Semi
major axis
(km)
Page 247
Perigee
height
(km)
Apogee
height
(km)
Orbital
Argument
eccentricity of perigee
(deg)
1970-113 A
[04813]
PLE
1970 Dec 18.68
12029 days
2003 Nov 24
Cylinder
2 vanes
2500?
5 long?
1.5 dia?
1970 Dec 25.3
2002 Dec 22.38
81.19
81.13
98.06
92.78
7043
6790
642
406
687
417
0.003
0.0008
270
168
Cosmos 389
1970-113 B
Block E 3rd stage [04814]
1970 Dec 18.68
60 years
Cylinder
1440
3.8 long
2.6 dia
1970 Dec 29.7
2002 Dec 21.79
81.20
81.17
98.08
95.47
7044
6920
602
510
729
573
0.009
0.005
172
144
D
Fragment
1970-113 C
[04834]
1972 Sep 19
641 days
D
Molniya-1 17
[Molniya 8K78M]
1970-114 A
[04829]
BAI
1970 Dec 25.16
31 months
1973 Jul
Windmill
6 vanes
1000?
3.4 long
1.6 dia
1970 Dec 28.7
1971 Feb 1.0
1972 Jul 1.0
64.99
64.99
65.00
711.80
717.75
720.96
26408
26556
26635
495
474
429
39565
39881
40085
0.740
0.742
0.744
285
-
D
Molniya-1 17
1970-114 B
Block I 3rd stage [04830]
1970 Dec 25.16
29 days
1971 Jan 23
Cylinder
2500?
7.5 long
2.6 dia
1970 Dec 26.7
65.01
91.10
6707
230
428
0.015
63
D
Molniya-1 17
4th stage casing
1970-114 C
[04831]
1970 Dec 25.16
47.12 days
1971 Feb 10.28
Irregular
-
1970 Dec 28.5
64.98
91.65
6734
240
472
0.017
70
D
Molniya-1 17
Ullage motor
1970-114 D
[04832]
1970 Dec 25.16
8 days
1971 Jan 2
D
Molniya-1 17
Ullage motor
1970-114 E
[04833]
1970 Dec 25.16
8 days
1971 Jan 2
D
Molniya-1 17
1970-114 F
Block L 4th stage [04837]
1970 Dec 25.16
799 days
1973 Mar 3
Cylinder
440
2.0 long
2.0 die
1971 Jan
1971 Sep
1972 Jun
65.02
64.99
65.02
709.66
709.66
709.48
26356
26356
26351
366
500
327
39589
39455
39619
0.744
0.739
0.745
285
-
D
Fragment
[06313]
1973 Feb 7
775 days
2014 – version 1.13
1970-114 G
3.6
1.0
1.0
RAE Table of Earth Satellites
Year of Launch 1970
Cospar ID
[Norad number]
Descent date
Lifetime
Date of
orbital
determination
Orbital
Inclination
(deg)
Nodal
period
(min)
(Revised 2002)
Extra Page 1970 - 1
Semi
major axis
(km)
Apogee
height
(km)
Perigee
height
(km)
Orbital
Argument
eccentricity 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 320 Cosmos 2 2nd stage fragments, 5 pieces, all have decayed
Analyses indicate that the Cosmos 2 2nd stage is the most likely debris source.
1970-05 C
[04303]
1970 Jan 24
8 days
1970-05 D
[04304]
1970 Feb 11
25 days
1970-05 E
[04305]
1970 Mar 3
46 days
1970-05 F
[04306]
1970 Jan 24
8 days
1970-05 G
[04307]
1970 Jan 29
13 days
Nimbus 4 Agena D stage fragments, 374 pieces, 125 have decayed
Fragment NL decayed by Norad, but still in orbit, based on the last elements from OIG.
This was the second Agena D stage to fragment in a span of only 12 months. The event occurred 1970 Oct 17 at
successful deployment of the Nimbus 4 payload. Twice in 1985, again in 1986, once in 1991, and twice in 1995
fragments, accounting for an additional 16 new debris objects between the 6 sub-events.
D 1970-25 D
[04601]
2000 Apr 20
10970 days
D 1970-25 E
[04602]
1982 Oct 14
4572 days
1970-25 F
[04603]
2002 Dec 17.63
100.22
D 1970-25 G
[04604]
1994 Feb 4
8703 days
D 1970-25 H
[04605]
1986 Aug 11
5969 days
D 1970-25 J
[04606]
1979 Aug 14
3415 days
1970-25 K
[04607]
2002 Dec 15.55
100.16
D 1970-25 L
[04608]
1992 Jan 26
7963 days
D 1970-25 M
[04609]
1991 May 5
7707 days
D 1970-25 N
[04610]
1999 Jan 1
10495 days
1970-25 P
[04611]
2002 Dec 15.96
99.82
1970-25 Q
[04612]
2000 Dec 15.65
99.75
1970-25 R
[04613]
2002 Dec 16.02
98.76
1970-25 S
[04614]
2002 Dec 18.41
100.08
1970-25 T
[04615]
2002 Dec 15.73
100.14
1970-25 U
[04636]
2002 Dec 15.89
99.96
1970-25 V
[04637]
2002 Dec 15.66
99.87
1970-25 W
[04638]
2002 Dec 15.99
99.98
1970-25 X
[04639]
2002 Dec 15.78
99.98
1970-25 Y
[04640]
2002 Dec 21.72
100.00
D 1970-25 Z
[04641]
1996 Sep 21
9663 days
D 1970-25 AA
[04642]
2013 Jun 12
15771 days
2002 Dec 21.58
99.96
2013 Jun 12.79
99.84
1970-25 AB
[04643]
2002 Dec 21.95
100.05
1970-25 AC
[04644]
2002 Dec 21.35
99.74
1970-25 AD
[04645]
2002 Dec 22.01
99.86
D 1970-25 AE
[04646]
1991 Oct 25
7870 days
D 1970-25 AF
[04647]
2001 Jan 11
11236 days
1970-25 AG
[04648]
2002 Dec 22.06
99.81
1970-25 AH
[04649]
2002 Dec 21.33
99.85
1970-25 AJ
[04650]
2002 Dec 20.53
99.90
2014 – version 1.13
03:17 UT near 50ºS 142ºE, six months after the
Nimbus 4 R/B debris spawned a few additional
106.58
7447
1042
1095
0.004
223
117.15
7931
1059
2046
0.062
235
103.05
103.40
102.45
104.12
105.20
105.47
105.78
102.28
108.15
107.92
7282
7298
7253
7332
7382
7395
7410
7245
7520
7509
798
848
788
891
959
989
1013
846
1055
1038
1009
992
962
1016
1049
1044
1050
888
1228
1223
0.014
0.010
0.012
0.009
0.006
0.004
0.003
0.003
0.012
0.012
158
355
64
164
232
257
80
18
83
108
100.42
88.57
106.43
106.17
112.05
7157
6582
7440
7427
7699
766
195
1055
1040
1066
791
211
1069
1058
1576
0.002
0.001
0.001
0.001
0.033
86
260
310
178
77
97.90
99.32
102.85
7037
7105
7272
587
638
805
731
816
982
0.010
0.013
0.012
317
97
275
RAE Table of Earth Satellites
Year of Launch 1970
Cospar ID
D
D
D
D
D
D
D
D
D
D
[Norad number]
1970-25
1970-25
1970-25
1970-25
1970-25
1970-25
1970-25
1970-25
1970-25
1970-25
AK
AL
AM
AN
AP
AQ
AR
AS
AT
AU
[04651]
[04652]
[04653]
[04654]
[04655]
[04656]
[04657]
[04658]
[04659]
[04660]
1970-25
1970-25
1970-25
1970-25
1970-25
1970-25
1970-25
1970-25
1970-25
1970-25
1970-25
1970-25
1970-25
1970-25
1970-25
1970-25
1970-25
1970-25
1970-25
1970-25
1970-25
1970-25
1970-25
1970-25
1970-25
1970-25
1970-25
1970-25
1970-25
1970-25
1970-25
1970-25
1970-25
1970-25
1970-25
1970-25
1970-25
AV
AW
AX
AY
AZ
BA
BB
BC
BD
BE
BF
BG
BH
BJ
BK
BL
BM
BN
BP
BQ
BR
BS
BT
BU
BV
BW
BX
BY
BZ
CA
CB
CC
CD
CE
CF
CG
CH
[04672]
[04673]
[04674]
[04675]
[04676]
[04677]
[04678]
[04679]
[04680]
[04681]
[04682]
[04683]
[04684]
[04685]
[04686]
[04687]
[04688]
[04689]
[04701]
[04702]
[04703]
[04704]
[04705]
[04706]
[04707]
[04708]
[04709]
[04710]
[04715]
[04716]
[04717]
[04718]
[04719]
[04720]
[04732]
[04733]
[04734]
2014 – version 1.13
Descent date
Lifetime
2013 May 2
15730 days
1982 Aug 13
4510 days
1980 Feb 20
3605 days
1988 Dec 16
6827 days
1990 Aug 8
1972
1972
1978
1992
Jul
Jul
Dec
Jan
22
7
1
27
1983 Oct 14
1972 Feb 6
(Revised 2002)
Extra Page 1970 - 2
Semi
major axis
(km)
Perigee
height
(km)
Apogee
height
(km)
Orbital
Argument
eccentricity of perigee
(deg)
103.72
104.43
102.20
103.35
105.40
105.52
105.42
104.32
104.60
100.47
90.47
106.45
101.10
7312
7346
7242
7296
7392
7397
7392
7341
7354
7159
6676
7441
7189
894
943
838
890
972
1001
1002
948
965
771
278
1033
740
974
993
889
945
1055
1036
1026
978
987
790
317
1092
882
0.005
0.003
0.004
0.004
0.006
0.002
0.002
0.002
0.002
0.001
0.003
0.004
0.010
10
193
27
7
241
2
130
29
168
221
279
194
101
99.99
100.07
100.17
106.60
106.37
106.13
7447
7437
7426
1068
1058
1040
1070
1059
1056
0.0001
0.0001
0.001
235
322
219
2002 Dec 20.65
100.15
105.62
7402
1010
1038
0.002
146
2002 Dec 21.69
2002 Dec 21.60
2002 Dec 21.84
99.89
999.77
100.02
110.28
108.93
108.15
7619
7556
7520
1053
1059
1047
1428
1297
1236
0.025
0.016
0.013
260
225
215
2002
2002
2002
2002
2002
21.19
21.07
22.52
21.37
20.08
100.04
100.33
100.17
100.20
100.13
106.47
106.38
106.75
106.58
106.45
7442
7438
7454
7447
7441
1023
1031
1054
1053
1010
1104
1088
1098
1085
1115
0.005
0.004
0.003
0.002
0.007
279
300
295
74
189
2002 Dec 22.12
2002 Dec 21.89
100.12
100.06
106.38
107.07
7437
7470
1025
1066
1093
1117
0.005
0.003
249
16
2002
2002
2002
2002
2002
2002
2002
2002
2002
20.52
21.10
20.26
20.42
20.62
20.42
21.15
18.55
21.87
100.10
100.06
99.94
99.53
99.98
100.13
100.06
100.00
99.99
105.07
100.93
106.38
104.38
103.85
106.42
103.07
103.58
103.22
7376
7182
7438
7344
7319
7439
7282
7306
7289
940
721
1056
937
932
1058
822
834
839
1055
886
1064
995
949
1063
986
1022
983
0.008
0.011
0.0005
0.004
0.001
0.0003
0.011
0.013
0.010
217
345
128
119
25
137
77
234
140
2002 Dec 21.27
2002 Dec 21.52
99.89
100.17
100.17
104.33
7144
7342
662
900
870
1027
0.015
0.009
325
216
Date of
orbital
determination
Orbital
Inclination
(deg)
Nodal
period
(min)
2002
2002
2002
2002
2002
2002
2002
2002
2002
2002
2013
2002
2002
21.21
21.73
21.23
21.82
22.14
21.59
20.26
20.57
21.28
21.92
2.16
22.07
21.03
100.12
99.52
100.02
100.02
100.08
99.81
100.08
100.00
100.10
100.07
99.96
100.13
99.07
2002 Dec 18.07
2002 Dec 21.98
2002 Dec 21.59
Dec
Dec
Dec
Dec
Dec
Dec
Dec
Dec
Dec
Dec
May
Dec
Dec
7427 days
Dec
Dec
Dec
Dec
Dec
837 days
822 days
3159 days
7964 days
4937 days
Dec
Dec
Dec
Dec
Dec
Dec
Dec
Dec
Dec
669 days
RAE Table of Earth Satellites
Year of Launch 1970
Cospar ID
D
D
D
D
D
D
1970-25
1970-25
1970-25
1970-25
1970-25
1970-25
1970-25
1970-25
1970-25
1970-25
1970-25
1970-25
1970-25
1970-25
1970-25
1970-25
1970-25
1970-25
1970-25
1970-25
1970-25
1970-25
1970-25
1970-25
1970-25
1970-25
1970-25
1970-25
1970-25
1970-25
1970-25
1970-25
1970-25
1970-25
1970-25
1970-25
1970-25
1970-25
1970-25
1970-25
1970-25
1970-25
1970-25
1970-25
1970-25
1970-25
1970-25
1970-25
[Norad number]
CJ
CK
CL
CM
CN
CP
CQ
CR
CS
CT
CU
CV
CW
CX
CY
CZ
DA
DB
DC
DD
DE
DF
DG
DH
DJ
DK
DL
DM
DN
DP
DQ
DR
DS
DT
DU
DV
DW
DX
DY
DZ
EA
EB
EC
ED
EE
EF
EG
EH
2014 – version 1.13
[04735]
[04736]
[04737]
[04738]
[04739]
[04740]
[04741]
[04742]
[04743]
[04744]
[04745]
[04746]
[04748]
[04749]
[04750]
[04751]
[04752]
[04753]
[04754]
[04755]
[04756]
[04757]
[04758]
[04759]
[04764]
[04765]
[04766]
[04767]
[04768]
[04769]
[04770]
[04771]
[04772]
[04773]
[04774]
[04775]
[04776]
[04777]
[04778]
[04818]
[04819]
[04820]
[04821]
[04822]
[04842]
[04851]
[04852]
[04853]
Descent date
1975 Aug 10
1990 Aug 23
1982 Mar 18
1989 May 16
1983 Feb 22
1981 Jul 31
Lifetime
(Revised 2002)
Extra Page 1970 - 3
Semi
major axis
(km)
Perigee
height
(km)
Apogee
height
(km)
Orbital
Argument
eccentricity of perigee
(deg)
7193
7294
7283
7293
7344
763
846
879
876
964
866
985
931
954
968
0.007
0.010
0.004
0.005
0.0003
76
325
271
176
245
120.67
106.50
106.32
106.27
104.15
101.42
105.92
104.92
8089
7443
7434
7433
7333
7204
7416
7369
1072
1050
1033
1042
933
819
1033
977
2350
1079
1079
1067
977
833
1042
1004
0.079
0.002
0.003
0.002
0.003
0.001
0.0006
0.002
270
38
43
232
115
197
331
225
100.10
99.93
99.97
99.63
100.12
100.09
99.76
104.82
103.50
104.95
103.47
104.50
106.83
105.97
7364
7303
7371
7302
7350
7459
7419
980
913
989
901
967
1058
1030
991
936
996
946
976
1103
1051
0.0008
0.002
0.0005
0.003
0.0006
0.003
0.001
155
76
81
340
300
178
147
21.62
21.21
22.32
21.67
22.03
21.54
21.23
99.97
99.57
99.58
100.02
100.06
100.21
99.61
105.33
103.83
100.73
106.30
105.15
105.30
100.72
7388
7318
7172
7434
7380
7387
7171
1009
906
731
1048
962
986
741
1011
974
857
1063
1042
1032
844
0.0002
0.005
0.009
0.001
0.005
0.003
0.007
138
112
358
339
133
79
225
2002 Dec 22.16
2002 Dec 21.65
2002 Dec 22.17
99.75
100.04
99.78
109.07
106.48
105.42
7562
7442
7392
1049
1039
979
1319
1089
1049
0.018
0.003
0.005
44
267
255
2002
2002
2002
2002
2002
2002
2002
2002
2002
2002
2002
2002
100.14
99.94
99.64
99.87
100.07
99.69
100.04
99.43
99.92
99.88
99.72
99.73
104.20
104.75
106.43
110.13
103.05
102.98
106.23
103.93
103.95
101.57
100.65
100.25
7336
7362
7440
7612
7281
7278
7431
7323
7324
7211
7168
7149
945
974
1035
1031
859
876
1044
893
925
826
763
744
970
993
1089
1436
947
924
1061
996
967
839
817
797
0.02
0.001
0.004
0.027
0.006
0.003
0.001
0.007
0.003
0.0009
0.004
0.004
166
22
114
122
140
161
359
63
332
14
289
132
Date of
orbital
determination
Orbital
Inclination
(deg)
Nodal
period
(min)
2002
2002
2002
2002
2002
Dec
Dec
Dec
Dec
Dec
22.21
20.86
21.54
21.09
22.32
99.67
100.09
99.22
100.13
99.92
101.18
103.30
103.10
103.30
104.38
2002
2002
2002
2002
2002
2002
2002
2002
Dec
Dec
Dec
Dec
Dec
Dec
Dec
Dec
21.56
20.08
21.67
20.25
21.67
22.06
21.45
21.54
100.24
100.20
100.00
99.95
100.10
100.03
100.12
99.71
2002
2002
2002
2002
2002
2002
2002
Dec
Dec
Dec
Dec
Dec
Dec
Dec
22.29
20.65
21.31
22.12
22.24
22.23
21.86
2002
2002
2002
2002
2002
2002
2002
Dec
Dec
Dec
Dec
Dec
Dec
Dec
855 days
7442 days
4362 days
6978 days
4703 days
4132 days
Dec
Dec
Dec
Dec
Dec
Dec
Dec
Dec
Dec
Dec
Dec
Dec
21.49
20.65
21.84
22.21
20.79
21.67
22.17
22.18
21.43
21.77
21.10
22.22
RAE Table of Earth Satellites
Year of Launch 1970
Cospar ID
D
D
D
D
D
D
D
D
D
D
D
D
D
D
D
[Norad number]
1970-25
1970-25
1970-25
1970-25
1970-25
1970-25
1970-25
1970-25
1970-25
1970-25
1970-25
1970-25
1970-25
1970-25
1970-25
1970-25
1970-25
1970-25
1970-25
EJ
EK
EL
EM
EN
EP
EQ
ER
ES
ET
EU
EV
EW
EX
EY
EZ
FA
FB
FC
[04854]
[04855]
[04856]
[04857]
[04858]
[04859]
[04860]
[04861]
[04862]
[04863]
[04864]
[04865]
[04866]
[04867]
[04868]
[04869]
[04870]
[04871]
[04877]
1970-25
1970-25
1970-25
1970-25
1970-25
1970-25
1970-25
1970-25
1970-25
1970-25
1970-25
1970-25
1970-25
1970-25
1970-25
1970-25
1970-25
1970-25
1970-25
1970-25
1970-25
1970-25
1970-25
1970-25
1970-25
1970-25
1970-25
1970-25
FD
FE
FF
FG
FH
FJ
FK
FL
FM
FN
FP
FQ
FR
FS
FT
FU
FV
FW
FX
FY
FZ
GA
GB
GC
GD
GE
GF
GG
[04898]
[04899]
[04908]
[04910]
[04911]
[04912]
[04913]
[04914]
[04915]
[04916]
[049]17
[049]18
[049]19
[04920]
[04921]
[04928]
[04929]
[04930]
[04931]
[04932]
[04933]
[04934]
[04935]
[04936]
[04943]
[04944]
[04945]
[04946]
2014 – version 1.13
Descent date
Lifetime
1979 May 23
3332 days
1990 May 6
7333 days
2001 Oct 26
11524 days
1981 Oct 26
2003 Jan 27
4219 days
11982 days
1999 Dec 21
1979 Nov 9
10849 days
3502 days
2013 Feb 5
15644 days
1982 Jun 1 A
2002 Apr 22
1991 Oct 27
4446 days
11702 days
7817 days
1971 Aug 8
Extra Page 1970 - 4
Semi
major axis
(km)
Perigee
height
(km)
Apogee
height
(km)
Orbital
Argument
eccentricity of perigee
(deg)
106.33
105.30
102.53
102.60
7435
7387
7257
7260
1044
995
760
837
1070
1022
997
926
0.002
0.002
0.016
0.006
20
316
324
318
99.99
106.37
7437
1019
1099
0.005
34
2002 Dec 21.52
99.73
100.48
7160
756
807
0.004
202
2002 Dec 22.17
2002 Dec 21.18
99.70
99.54
98.93
106.87
7086
7460
693
1047
723
1117
0.002
0.005
120
289
2002 Dec 22.46
2002 Dec 20.79
2002 Dec 22.13
99.69
99.59
99.73
94.30
103.17
103.72
6864
7287
7313
480
806
888
491
1012
981
0.0008
0.014
0.006
202
234
281
2002 Dec 22.19
2002 Dec 22.49
2013 Feb 4.71
99.75
99.70
99.61
100.53
99.03
88.72
7162
7091
6590
757
688
204
811
738
218
0.004
0.004
0.001
229
230
289
2002
2002
2002
2002
2002
Dec
Dec
Dec
Dec
Dec
21.40
22.44
21.48
21.06
20.90
99.43
99.99
99.78
99.90
99.45
104.43
102.17
102.73
103.15
105.57
7346
7240
7267
7286
7400
874
803
852
805
953
1061
920
925
1011
1090
0.013
0.008
0.005
0.014
0.009
18
173
86
139
131
2002
2002
2002
2002
2002
2002
2002
2002
Dec
Dec
Dec
Dec
Dec
Dec
Dec
Dec
21.49
21.78
22.07
21.20
20.64
22.03
20.57
21.45
99.67
99.72
99.45
100.06
99.45
99.78
99.71
99.66
98.72
100.28
108.67
103.00
107.05
101.92
113.52
114.17
7076
7151
7544
7279
7434
7228
7766
7796
673
742
1040
864
1021
802
1042
1057
723
803
1291
938
1160
897
1734
1778
0.004
0.004
0.017
0.005
0.009
0.007
0.045
0.046
172
144
136
155
176
91
133
31
2002 Dec 22.22
99.75
104.73
7360
958
1006
0.003
129
2002 Dec 22.41
2002 Dec 22.34
100.08
99.87
105.27
104.45
7385
7347
1002
918
1012
1020
0.0007
0.007
28
40
2002 Dec 21.90
99.66
110.05
7608
1054
1405
0.023
249
2002 Dec 21.21
2002 Dec 21.01
99.84
99.72
105.00
105.00
7373
7373
915
981
1075
1008
0.011
0.002
93
284
Orbital
Inclination
(deg)
Nodal
period
(min)
2002
2002
2002
2002
100.08
99.95
99.77
99.74
2002 Dec 22.09
Dec
Dec
Dec
Dec
21.04
20.70
21.10
21.22
487 days
2000 Oct 19
1978 Aug 4
11152 days
3040 days
1979 Jun 8
3348 days
1980 Jul 22
(Revised 2002)
Date of
orbital
determination
3758 days
RAE Table of Earth Satellites
Year of Launch 1970
Cospar ID
D
D
D
D
D
D
D
D
D
D
D
D
D
D
D
D
D
D
D
1970-25
1970-25
1970-25
1970-25
1970-25
1970-25
1970-25
1970-25
1970-25
1970-25
1970-25
1970-25
1970-25
1970-25
1970-25
1970-25
1970-25
1970-25
1970-25
1970-25
1970-25
1970-25
1970-25
1970-25
1970-25
1970-25
1970-25
1970-25
1970-25
1970-25
1970-25
1970-25
1970-25
1970-25
1970-25
1970-25
1970-25
1970-25
1970-25
1970-25
1970-25
1970-25
1970-25
1970-25
1970-25
1970-25
1970-25
1970-25
[Norad number]
GH
GJ
GK
GL
GM
GN
GP
GQ
GR
GS
GT
GU
GV
GW
GX
GY
GZ
HA
HB
HC
HD
HE
HF
HG
HH
HJ
HK
HL
HM
HN
HP
HQ
HR
HS
HT
HU
HV
HW
HX
HY
HZ
JA
JB
JC
JD
JE
JF
JG
2014 – version 1.13
[04947]
[04948]
[04949]
[04950]
[04951]
[04968]
[04969]
[04970]
[049]71
[04972]
[04973]
[04974]
[04975]
[04976]
[04977]
[04978]
[04979]
[04980]
[04981]
[04982]
[04983]
[04984]
[04985]
[04986]
[04987]
[04988]
[04989]
[04990]
[04991]
[04992]
[04993]
[04994]
[04995]
[04996]
[04997]
[04998]
[04999]
[05000]
[05023]
[05024]
[05025]
[05026]
[05027]
[05037]
[05038]
[05060]
[05061]
[05062]
Descent date
Lifetime
1981 Jul 18
4119 days
1972 Mar 5
697 days
1997 Jul 8
416 days
1971 Jul 2
1978 Jun 2
2002 Feb 25
450 days
2977 days
11646 days
1981 Apr 13
4023 days
1999 Dec 23
10851 days
2001 Oct 10
1972 Apr 11
2000 Jun 9
11508 days
734 days
11020 days
12637 days
7117 days
1979 Oct 28 A
3490 days
1979 Sep 29
3461 days
1991 Jan 17
1980 Jul 18
1971 Jul 18
2002 May 10
Extra Page 1970 - 5
Semi
major axis
(km)
Perigee
height
(km)
Apogee
height
(km)
Orbital
Argument
eccentricity of perigee
(deg)
7487
941
1276
0.022
179
110.03
106.00
105.90
7607
7419
7416
1060
1026
1022
1397
1056
1053
0.022
0.002
0.002
353
223
177
100.01
99.93
106.23
112.33
7431
7712
1024
1065
1081
1603
0.004
0.035
108
307
2002 Dec 16.43
100.04
103.50
7303
860
989
0.009
145
2002 Dec 15.67
100.08
106.57
7446
1052
1083
0.002
100
2002 Dec 15.66
2002 Dec 16.01
99.97
99.99
106.07
106.02
7423
7420
1036
1035
1053
1049
0.001
0.001
244
222
2002 Dec 16.18
99.70
107.57
7492
1055
1173
0.008
330
2002
2002
2002
2002
2002
2002
2002
2002
2002
15.90
15.09
15.58
16.08
15.12
15.79
15.16
16.02
16.01
100.28
99.43
99.98
99.64
100.01
99.97
99.98
100.21
99.72
107.32
106.82
105.85
106.37
104.07
106.42
105.98
103.53
97.68
7481
7458
7413
7437
7329
7439
7419
7304
7026
1063
1051
1024
954
903
1046
1029
853
632
1143
1109
1046
1163
999
1076
1052
999
664
0.005
0.004
0.001
0.014
0.007
0.002
0.002
0.010
0.002
297
265
296
4
15
345
179
293
309
2002 Dec 15.65
2002 Dec 16.14
2002 Dec 16.32
100.36
99.95
100.03
104.08
103.72
106.47
7330
7313
7441
884
892
1056
1020
977
1070
0.009
0.006
0.001
180
201
1
2002 Dec 15.41
99.78
113.83
7781
1010
1795
0.050
23
2002 Dec 16.15
2002 Dec 16.09
2002 Dec16.46
99.84
100.20
100.24
102.25
106.87
105.55
7244
7460
7398
792
1048
992
940
1116
1048
0.010
0.005
0.004
30
116
123
2002 Dec 16.15
2002 Dec 16.18
100.02
99.69
102.20
100.27
7241
7149
748
746
978
796
0.016
0.003
170
153
Orbital
Inclination
(deg)
Nodal
period
(min)
2002 Dec 21.45
99.43
107.45
2002 Dec 21.23
2002 Dec 20.99
2002 Dec 21.40
99.82
100.12
100.12
2002 Dec 15.14
2002 Dec 16.19
9952 days
1971 May 29
2004 Nov 12
1989 Oct 2
(Revised 2002)
Date of
orbital
determination
Dec
Dec
Dec
Dec
Dec
Dec
Dec
Dec
Dec
7589 days
3754 days
466 days
11720 days
RAE Table of Earth Satellites
Year of Launch 1970
Cospar ID
D
D
D
D
D
D
D
D
D
D
D
D
D
D
[Norad number]
1970-25
1970-25
1970-25
1970-25
1970-25
1970-25
1970-25
JH
JJ
JK
JL
JM
JN
JP
[05063]
[05064]
[05065]
[05066]
[05067]
[05129]
[05133]
1970-25
1970-25
1970-25
1970-25
1970-25
1970-25
1970-25
1970-25
1970-25
1970-25
1970-25
JQ
JR
JS
JT
JU
JV
JW
JX
JY
JZ
KA
[05146]
[05148]
[05149]
[05150]
[05151]
[05152]
[05153]
[05154]
[05165]
[05183]
[05184]
1970-25
1970-25
1970-25
1970-25
1970-25
1970-25
1970-25
1970-25
1970-25
1970-25
1970-25
1970-25
1970-25
1970-25
1970-25
1970-25
1970-25
1970-25
1970-25
1970-25
1970-25
1970-25
1970-25
1970-25
1970-25
1970-25
1970-25
1970-25
KB
KC
KD
KE
KF
KG
KH
KJ
KK
KL
KM
KN
KP
KQ
KR
KS
KT
KU
KV
KW
KX
KY
KZ
LA
LB
LC
LD
LE
[05185]
[05186]
[05190]
[05203]
[05219]
[05220]
[05226]
[05266]
[05346]
[05347]
[05348]
[05349]
[05350]
[05359]
[05386]
[05387]
[05388]
[05389]
[05390]
[05391]
[05392]
[05393]
[05421]
[05422]
[05423]
[05424]
[05445]
[05446]
2014 – version 1.13
Descent date
Lifetime
2005 Aug 20
1984 Jan 30
12918 days
5045 days
2012 Nov 16
15563 days
1991 Mar 13
7644 days
2014 Apr 14
16077 days
1979 Nov 10
3503 days
1988 Oct 28
6778 days
1971 Oct 14
189 days
1992 Mar 5
8002 days
1982 Feb 16
4332 days
2001 Apr 24
1979 Aug 29
11339 days
3430 days
1971 Dec 5
1982 Mar 19
1988 Oct 28
606 days
4363 days
6778 days
(Revised 2002)
Extra Page 1970 - 6
Semi
major axis
(km)
Perigee
height
(km)
Apogee
height
(km)
Orbital
Argument
eccentricity of perigee
(deg)
7260
7036
866
639
898
677
0.002
0.003
345
243
103.48
105.82
107.53
99.23
87.87
105.80
95.40
102.48
104.55
105.88
7302
7411
7491
7100
6548
7410
6917
7255
7352
7414
871
1029
945
703
162
1000
532
827
900
1035
976
1037
1280
741
176
1064
545
927
1048
1037
0.007
0.0006
0.022
0.003
0.001
0.004
0.001
0.007
0.010
0.0001
350
162
300
82
121
301
87
122
160
300
100.08
99.87
99.71
100.07
99.39
99.33
99.60
99.98
106.43
102.00
100.48
105.00
98.85
90.32
104.75
99.65
7440
7232
7160
7373
7082
6669
7361
7120
1036
850
756
970
658
281
925
709
1088
857
807
1020
750
299
1040
775
0.004
0.0005
0.004
0.003
0.007
0.001
0.008
0.005
262
297
195
278
309
186
161
308
2002 Dec 16.35
99.85
109.80
7596
1043
1393
0.023
195
2002 Dec 16.46
2002 Dec 16.44
2002 Dec 16.37
99.83
99.68
99.69
112.12
96.62
98.73
7702
6975
7076
1032
586
675
1616
607
721
0.038
0.002
0.003
6
252
330
2002 Dec 16.10
99.98
104.47
7348
934
1006
0.005
173
2002
2002
2002
2002
2002
2002
2002
2002
16.20
16.41
16.11
16.16
15.98
16.37
15.59
15.25
99.83
99.70
100.02
99.65
100.92
99.83
99.82
100.03
104.33
98.92
105.45
99.87
120.17
108.12
109.90
104.72
7342
7086
7394
7130
8067
7518
7601
7359
903
682
1013
726
1429
1032
1067
938
1025
733
1019
778
1948
1248
1379
1024
0.008
0.004
0.0004
0.004
0.032
0.014
0.021
0.006
3
13
221
141
201
279
312
142
2002 Dec 16.16
100.07
103.22
7290
872
951
0.005
177
2002 Dec 15.62
100.05
102.48
7255
784
969
0.013
217
2002 Dec 15.44
100.48
106.02
7421
973
1112
0.009
332
Date of
orbital
determination
Orbital
Inclination
(deg)
Nodal
period
(min)
2002 Dec 16.39
2002 Dec 16.04
99.88
99.69
102.60
97.88
2002
2002
2002
2002
2012
2002
2002
2002
2002
2002
Dec
Dec
Dec
Dec
Nov
Dec
Dec
Dec
Dec
Dec
15.53
15.12
16.06
16.27
15.75
16.22
16.04
16.46
16.11
15.58
99.91
100.02
99.29
99.68
99.61
99.88
99.66
99.67
99.55
100.13
2002
2002
2002
2002
2002
2014
2002
2002
Dec
Dec
Dec
Dec
Dec
Apr
Dec
Dec
16.16
16.24
16.18
16.13
16.06
13.76
15.73
15.96
Dec
Dec
Dec
Dec
Dec
Dec
Dec
Dec
RAE Table of Earth Satellites
Year of Launch 1970
Cospar ID
D
D
D
D
D
D
D
D
D
D
D
D
D
D
D
D
D
D
D
D
D
D
D
D
D
1970-25
1970-25
1970-25
1970-25
1970-25
1970-25
1970-25
1970-25
1970-25
1970-25
1970-25
1970-25
1970-25
1970-25
1970-25
1970-25
1970-25
1970-25
1970-25
1970-25
1970-25
1970-25
1970-25
1970-25
1970-25
1970-25
1970-25
1970-25
1970-25
1970-25
1970-25
1970-25
1970-25
1970-25
1970-25
1970-25
1970-25
1970-25
1970-25
1970-25
1970-25
1970-25
1970-25
1970-25
1970-25
1970-25
1970-25
1970-25
[Norad number]
LF
LG
LH
LJ
LK
LL
LM
LN
LP
LQ
LR
LS
LT
LU
LV
LW
LX
LY
LZ
MA
MB
MC
MD
ME
MF
MG
MH
MJ
MK
ML
MM
MN
MP
MQ
MR
MS
MT
MU
MV
MW
MX
MY
MZ
NA
NB
NC
ND
NE
2014 – version 1.13
[05501]
[05502]
[05504]
[05505]
[05506]
[05507]
[05508]
[05509]
[05510]
[05535]
[05600]
[05601]
[05621]
[05622]
[05690]
[05691]
[05692]
[05693]
[05694]
[05695]
[05696]
[05697]
[05698]
[05699]
[05700]
[05701]
[05736]
[05824]
[05825]
[05842]
[05843]
[05957]
[05958]
[05967]
[06014]
[06015]
[06051]
[06084]
[06139]
[06140]
[06157]
[06159]
[06160]
[06161]
[06167]
[06184]
[06185]
[06216]
Descent date
Lifetime
1978 Dec 26
3184 days
1991 Jun 23
1991 Mar 20
1991 Mar 28
7746 days
7286 days
7294 days
1991
1972
1991
1972
1990
1988
1972
1991
7899 days
734 days
7284 days
716 days
7313 days
6793 days
713 days
7790 days
Nov
Apr
Mar
Mar
Apr
Nov
Mar
Aug
23
11
18
24
16
12
21
6
1991 Mar 29
7295 days
1984 Dec 13
5363 days
1991 Apr 1
7298 days
1989 Dec 15
1979 Jun 16
1990 Jan 27
7191 days
3356 days
7234 days
1972 Dec 3
970 days
1989 Feb 23
6896 days
1973 Feb 19
1976 Mar 17
1974 May 12
1048 days
2170 days
1495 days
1979 Mar 20
3268 days
1988 Oct 30
6780 days
1990 Nov 6
1981 Jun 8
7517 days
4079 days
(Revised 2002)
Extra Page 1970 - 7
Semi
major axis
(km)
Perigee
height
(km)
Apogee
height
(km)
Orbital
Argument
eccentricity of perigee
(deg)
7252
847
901
0.004
90
102.90
7274
868
924
0.004
273
99.43
99.27
99.47
106.68
103.72
106.58
7452
7313
7447
1036
909
982
1111
960
1156
0.005
0.004
0.012
87
290
262
2002 Dec 16.47
99.85
101.75
7220
810
874
0.004
192
2002 Dec 16.12
99.42
106.57
7446
1025
1111
0.006
212
2002 Dec 15.37
99.90
106.12
7425
1039
1055
0.001
249
2002 Dec 15.45
2002 Dec 16.37
101.43
97.88
109.98
108.95
7605
7557
1049
701
1404
1656
0.023
0.063
223
26
2002 Dec 15.82
100.03
100.85
7177
754
844
0.006
152
2002
2002
2002
2002
99.63
99.48
101.64
100.04
102.85
106.10
112.07
104.08
7272
7424
7700
7330
859
1006
1223
906
928
1086
1421
998
0.005
0.005
0.013
0.006
273
32
9
74
2002 Dec 16.01
99.47
104.08
7330
894
1010
0.008
155
2002 Dec 15.10
2002 Dec 15.52
2002 Dec 16.05
99.87
101.26
100.46
103.32
112.55
103.92
7294
7722
7322
907
1300
866
925
1387
1022
0.001
0.006
0.011
157
130
215
2002 Dec 15.37
100.02
105.67
7405
1002
1051
0.003
322
2002 Dec 15.55
99.11
101.35
7201
629
1017
0.027
72
Date of
orbital
determination
Orbital
Inclination
(deg)
Nodal
period
(min)
2002 Dec 15.57
99.57
102.43
2002 Dec 15.55
99.35
2002 Dec 14.57
2002 Dec 16.40
2002 Dec 15.11
dec
dec
Dec
Dec
15.81
15.70
15.76
16.06
RAE Table of Earth Satellites
Year of Launch 1970
Cospar ID
[Norad number]
Descent date
Lifetime
1970-25 NF
[06767]
2002 Dec
1970-25 NG
[06765]
2002 Dec
1970-25 NH
[06766]
2002 Dec
1970-25 NJ
[08908]
2002 Dec
1970-25 NK
[09666]
2002 Dec
D? 1970-25 NL
[09667]
1978 Apr 5 A?
2919 days?
1999 Aug
Fragment NL decayed by Norad, but still in orbit; based on the last elements from OIG.
1970-25 NM
[09668]
2002 Dec
D 1970-25 NN
[09784]
1989 Nov 21
7171 days
D 1970-25 NP
[09997]
1978 Jan 4
2828 days
1970-25 NQ
[10136]
2002 Dec
1970-25 NR
[13518]
2002 Dec
1970-25 NS
[14466]
2002 Dec
1970-25 NT
[14467]
2002 Dec
D 1970-25 NU
[14468]
1992 Jan 31
7968 days
1970-25 NV
[14469]
2002 Dec
1970-25 NW
[14478]
2002 Dec
D 1970-25 NX
[14479]
1990 Jan 4
7211 days
D 1970-25 NY
[15520]
1989 Jun 6
6999 days
D 1970-25 NZ
[15537]
1988 Dec 20
6831 days
1988 Dec
1970-25 PA
[16715]
2002 Dec
D 1970-25 PB
[17169]
1992 Feb 28
7996 days
D 1970-25 PC
[17170]
1995 Jul 23
9237 days
D 1970-25 PD
[17715]
2002 Sep 15
11848 days
1970-25 PE
[17716]
2002 Dec
1970-25 PF
[17717]
2002 Dec
D 1970-25 PG
[17718]
1989 Dec 22
7198 days
1970-25 PH
[17719]
2002 Dec
1970-25 PJ
[17720]
2002 Dec
D 1970-25 PK
[17721]
1989 Aug 17
7071 days
1970-25 PL
[18418]
2002 Dec
D 1970-25 PM
[18419]
1992 Jan 20
7957 days
1970-25 PN
[18513]
2002 Dec
D 1970-25 PP
[18547]
1999 Aug 5
10711 days
1970-25 PQ
[18785]
2002 Dec
D 1970-25 PR
[18811]
1989 Aug 14
7068 days
1970-25 PS
[19150]
2002 Dec
1970-25 PT
[19238]
2002 Dec
1970-25 PU
[19250]
2002 Dec
1970-25 PV
[19290]
2002 Dec
1970-25 PW
[19351]
2002 Dec
D 1970-25 PX
[19353]
1998 Mar 6
10194 days
1970-25 PY
[19363]
2002 Dec
1970-25 PZ
[19391]
2002 Dec
1970-25 QA
[19422]
2002 Dec
1970-25 QB
[19423]
2002 Dec
1970-25 QC
[19667]
2002 Dec
1970-25 QD
[19948]
2002 Dec
2014 – version 1.13
(Revised 2002)
Extra Page 1970 - 8
Semi
major axis
(km)
Perigee
height
(km)
Apogee
height
(km)
Orbital
Argument
eccentricity of perigee
(deg)
104.18
106.43
103.52
106.70
106.78
107.47
7334
7440
7304
7453
7456
7488
938
1050
863
942
981
1073
974
1074
988
1207
1175
1147
0.002
0.002
0.009
0.018
0.013
0.005
62
88
138
38
213
60
100.12
101.17
7193
752
877
0.009
208
16.90
19.24
20.32
19.13
99.98
100.01
99.98
100.06
106.57
105.02
101.73
105.87
7446
7374
7219
7414
1067
993
782
1034
1069
998
900
1037
0.0001
0.0004
0.008
0.0002
180
305
200
292
19.44
20.16
101.68
100.78
110.33
117.32
7621
7939
1035
1120
1450
2001
0.027
0.055
121
76
17.29
19.07
99.43
100.09
94.37
106.02
6879
7420
471
1037
530
1047
0.004
0.0007
284
251
19.15
19.56
99.53
100.01
102.37
99.75
7249
7125
842
660
900
833
0.004
0.012
270
78
19.52
19.57
99.16
99.68
103.02
103.67
7279
7310
807
898
995
966
0.013
0.005
309
55
19.26
100.12
105.47
7395
1013
1020
0.0005
45
19.26
99.73
102.58
7260
834
929
0.007
288
19.24
100.01
106.05
7422
1041
1047
0.0004
40
20.09
21.16
19.68
21.05
19.62
100.35
99.79
99.42
100.05
100.08
105.40
105.53
106.35
106.28
105.33
7392
7398
7436
7433
7389
980
988
905
1035
989
1047
1051
1210
1075
1032
0.004
0.004
0.020
0.003
0.003
247
98
180
79
319
20.91
19.96
20.87
19.27
20.51
19.89
100.10
98.75
100.13
99.80
99.70
99.58
105.98
104.05
105.75
101.35
112.43
113.17
7419
7329
7408
7201
7717
7750
1036
828
1021
770
1073
1046
1045
1073
1039
876
1605
1698
0.0007
0.017
0.001
0.007
0.034
0.042
196
359
185
71
347
42
Date of
orbital
determination
Orbital
Inclination
(deg)
Nodal
period
(min)
15.09
16.12
16.22
15.48
15.42
24.10
99.35
100.12
100.14
101.65
99.25
100.52
15.80
RAE Table of Earth Satellites
Year of Launch 1970
Cospar ID
D
D
D
D
D
D
D
1970-25
1970-25
1970-25
1970-25
1970-25
1970-25
1970-25
1970-25
1970-25
1970-25
1970-25
1970-25
1970-25
[Norad number]
QE
QF
QG
QH
QJ
QK
QL
QM
QN
QP
QQ
QR
QS
[20326]
[20360]
[21721]
[21837]
[21838]
[21839]
[21840]
[21841]
[22532]
[22533]
[26821]
[35410]
[37864]
1970-25 QT
[39592]
Descent date
2001
2001
2001
2001
2001
Sep
Oct
Oct
Apr
Apr
Lifetime
28
4
13
3
19
2014 Dec 2
2014 Jan 8
11496
11502
11511
11318
11334
(Revised 2002)
Extra Page 1970 - 9
Semi
major axis
(km)
Perigee
height
(km)
Apogee
height
(km)
Orbital
Argument
eccentricity of perigee
(deg)
102.03
105.82
105.93
7233
7411
7417
802
1007
1032
908
1059
1045
0.007
0.004
0.0009
87
37
219
100.07
100.06
100.01
99.82
99.77
99.71
100.02
106.05
106.10
102.33
90.25
97.82
89.62
106.57
7422
7425
7248
6665
7033
6634
7446
1041
1043
803
276
586
253
1064
1046
1050
936
298
722
259
1070
0.0003
0.0004
0.009
0.002
0.010
0.0005
0.0004
159
219
106
325
171
203
308
2002 Dec 15.46
2002 Dec 16.46
90.01
89.97
102.05
109.00
7235
7559
834
940
879
1421
0.003
0.032
51
60
2002 Dec 21.02
89.99
99.92
7133
716
794
0.006
240
Date of
orbital
determination
Orbital
Inclination
(deg)
Nodal
period
(min)
2002 Dec 21.06
2002 Dec 19.56
2002 dec 21.03
99.92
100.46
100.13
2002
2002
2002
2014
2011
2014
2014
days
days
days
days
days
16309 days
15981 days
Transit 0-19 fragments, 4 pieces, 1 has decayed
One of several Transit-class satellites involved in anomalous events.
1970-67 C
[05036]
1970-67 D
[05447]
1970-67 E
[06372]
1981 Apr 13
3882 days
1970-67 F
[25830]
Dec
Dec
Dec
Dec
Nov
Jan
Mar
16.41
16.39
19.91
1.43
18.22
7.95
12.13
Cosmos 374 fragments, 101 pieces, 80 have decayed
In SSR 45-1 the ID’s for 1970 89 BK and BY were swapped with 1968 97 CQ and CY
Cosmos 374 was launched on a two-revolution rendezvous with Cosmos 373. After a close approach, Cosmos 374 continued on before its warhead was intentionally
fired 1970 Oct 23 at 15:13 UT near 22ºS 217ºE. Cosmos 374 was part of test series begun with Cosmos 249. Considerable cross-cataloging of Cosmos 374 and
Cosmos 375 debris occurred.
1970-89 C
[04616]
2002 Dec 16.38
62.82
113.63
7772
655
2132
0.095
217
1970-89 D
[04617]
2002 Dec 16.14
62.91
103.93
7323
486
1403
0.063
83
D 1970-89 E
[04618]
2000 Dec 23
11019 days
D 1970-89 F
[04619]
2000 Oct 9
10944 days
D 1970-89 G
[04620]
2001 Mar 11
11097 days
1970-89 H
[04621]
2002 Dec 15.59
62.91
108.03
7515
517
1756
0.082
68
D 1970-89 J
[04666]
1990 Sep 25
7277 days
1970-89 K
[04667]
2002 Dec 15.85
62.95
107.78
7504
553
1699
0.076
5
1970-89 L
[04668]
2002 Dec 16.21
62.98
112.00
7697
591
2047
0.095
322
D 1970-89 M
[04669]
1980 Aug 8 A
3577 days
D 1970-89 N
[04670]
1978 Apr 3
2719 days
D 1970-89 P
[04671]
1979 Jan 27
3018 days
1970-89 Q
[04698]
2002 Dec 15.74
63.13
108.33
7528
658
1642
0.065
333
1970-89 R
[04699]
2002 Dec 15.76
62.94
111.40
7669
554
2028
0.096
12
1970-89 S
[04711]
2002 Dec 15.75
63.16
108.78
7549
623
1719
0.073
318
1970-89 T
[04823]
2002 Dec 16.33
63.01
114.17
7796
652
2184
0.098
135
D 1970-89 U
[04824]
1979 Oct 21 A
3285 days
D 1970-89 V
[04825]
2004 May 6
12249 days
2002 Dec 15.78
62.84
96.43
6967
469
708
0.017
334
1970-89 W
[05020]
2002 Dec 15.42
62.92
108.33
7529
524
1777
0.083
51
D 1970-89 X
[05021]
2000 Apr 21
10773 days
2014 – version 1.13
RAE Table of Earth Satellites
Year of Launch 1970
Cospar ID
D
D
D
D
D
D
D
D
D
D
D
D
D
D
D
D
D
D
D
D
D
D
D
D
D
D
D
D
D
D
D
D
D
D
D
D
D
D
D
D
D
D
[Norad number]
Descent date
1970-89 Y
[05022]
1972 Jun 24
1970-89 Z
[05028]
1970-89 AA
[05029]
1981 Jun 3
1970-89 AB
[05031]
1990 Mar 30
1970-89 AC
[05032]
1983 Aug 14
1970-89 AD
[05033]
1990 Mar 1
1970-89 AE
[05034]
2001 Apr 14
1970-89 AF
[05068]
1976 Dec 5
1970-89 AG
[05069]
1972 Feb 22
1970-89 AH
[05070]
2000 Sep 28
1970-89 AJ
[05071]
1979 Oct 2
1970-89 AK
[05072]
1981 Apr 13
1970-89 AL
[05073]
1971 Jul 26
1970-89 AM
[05074]
1981 Apr 13
1970-89 AN
[05075]
1995 Oct 5
1970-89 AP
[05076]
1970-89 AQ
[05077]
2000 Nov 6
1970-89 AR
[05078]
1972 Apr 22
1970-89 AS
[05079]
1979 Mar 26 A
1970-89 AT
[05080]
1981 Jun 29
1970-89 AU
[05081]
1981 Oct 29
1970-89 AV
[05096]
1979 May 1
1970-89 AW
[05132]
1982 Nov 10
1970-89 AX
[05136]
1981 Nov 9
1970-89 AY
[05138]
1972 Mar 24
1970-89 AZ
[05188]
1970-89 BA
[05189]
1982 Nov 10 A
1970-89 BB
[05198]
2001 Nov 7
1970-89 BC
[05199]
1976 Dec 5
1970-89 BD
[05202]
1977 Aug 23
1970-89 BE
[05224]
1978 Dec 22
1970-89 BF
[05240]
1970-89 BG
[05242]
1992 Nov 17
1970-89 BH
[05276]
1979 Jun 16
1970-89 BJ
[05278]
1983 Mar 6
1970-89 BK
[R05515]
1982 Nov 22 A
Re-assigned to 1965-108 BJ per 2004-10-02
1970-89 BL
[05293]
1976 Dec 5
1970-89 BM
[05294]
1972 Feb 16
1970-89 BN
[05295]
1991 Dec 16
1970-89 BP
[05296]
1991 May 20
1970-89 BQ
[05321]
1976 Dec 5
1970-89 BR
[05335]
1979 Nov 20
1970-89 BS
[05337]
1970-89 BT
[05338]
1992 Jun 16
1970-89 BU
[05411]
1982 Jun 2
1970-89 BV
[05412]
1980 Apr 30
1970-89 BW
[05413]
1980 Jul 24
2014 – version 1.13
Lifetime
(Revised 2002)
Extra Page 1970 - 10
Semi
major axis
(km)
Perigee
height
(km)
Apogee
height
(km)
Orbital
Argument
eccentricity of perigee
(deg)
7647
583
1954
0.090
25
112.37
7714
578
2093
0.098
301
63.99
114.55
7813
721
2148
0.091
323
2002 Dec 15.71
62.85
113.10
7751
637
2108
0.095
102
2002 Dec 15.13
62.97
112.08
7701
701
1945
0.081
300
Date of
orbital
determination
Orbital
Inclination
(deg)
Nodal
period
(min)
2002 Dec 16.22
63.25
110.90
2002 Dec 16.55
62.81
2002 Dec 15.93
610 days
3876 days
7098 days
4525 days
7069 days
11131 days
2235 days
487 days
10933 days
3266 days
3825 days
276 days
3825 days
9090 days
10972 days
547 days
3076 days
3902 days
4024 days
3112 days
4401 days
4400 days
518 days
4401 days
11338 days
2235 days
2496 days
2982 days
8038
3158
4517
4413
days
days
days
days
2235 days
481 days
7724 days
7514 days
2235 days
3315 days
7907
4240
3477
3562
days
days
days
days
RAE Table of Earth Satellites
Year of Launch 1970
Cospar ID
D
D
D
D
D
D
D
D
D
D
D
D
D
D
D
D
D
D
D
D
D
D
D
D
D
D
D
D
[Norad number]
Descent date
1970-89 BX
[05431]
1972 Jan 26
1970-89 BY
[R05632]
1999 Jun 3
Re-assigned to 1965-108 BK per 2004-10-02
1970-89 BZ
[05433]
1982 Jan 1
1970-89 CA
[05454]
1980 Apr 21
1970-89 CB
[05455]
1975 Sep 3
1970-89 CC
[05456]
1977 Sep 3
1970-89 CD
[R05457]
Re-assigned to 1965-108 BG per 2004-10-02
1970-89 CE
[05458]
1976 Apr 12
1970-89 CF
[05523]
1981 Feb 24
1970-89 CG
[05524]
1979 Apr 7
1970-89 CH
[05525]
1990 Dec 14
1970-89 CJ
[05638]
2003 Jun 17
1970-89 CK
[05759]
2002 Jan 20
1970-89 CL
[05795]
1970-89 CM
[05796]
1972 Aug 6
1970-89 CN
[05797]
1974 May 5
1970-89 CP
[05896]
1973 Apr 2
1970-89 CQ
[05897]
1981 Jul 22
1970-89 CR
[05898]
1981 Nov 5
1970-89 CS
[05963]
1979 Jul 23
1970-89 CT
[06085]
2001 Jun 13
1970-89 CU
[06177]
1982 Jan 4
1970-89 CV
[13936]
1983 Oct 20
1970-89 CW
[14122]
1970-89 CX
[14834]
1984 May 8
1970-89 CY
[14835]
1984 Apr 21
1970-89 CZ
[14836]
1989 Apr 7
1970-89 DA
[15782]
1991 Dec 8
1970-89 DB
[17669]
1991 Aug 6
1970-89 DC
[17725]
1970-89 DD
[18517]
1970-89 DE
[19433]
1989 Sep 25
1970-89 DF
[19817]
1970-89 DG
[20049]
1989 Jun 15
Lifetime
(Revised 2002)
Extra Page 1970 - 11
Semi
major axis
(km)
Perigee
height
(km)
Apogee
height
(km)
Orbital
Argument
eccentricity of perigee
(deg)
7473
507
1683
0.078
258
95.25
6910
415
648
0.017
125
62.87
97.43
7015
465
808
0.024
157
2002 Dec 20.35
62.88
105.02
7374
500
1492
0.067
69
2002 Dec 19.57
2002 Dec 19.46
62.74
62.42
108.87
104.83
7553
7365
531
518
1819
1456
0.085
0.064
33
73
2002 Dec 21.04
62.22
93.38
6819
380
501
0.009
343
Date of
orbital
determination
Orbital
Inclination
(deg)
Nodal
period
(min)
2002 Dec 15.70
62.29
107.15
2002 Dec 15.62
62.46
2002 Dec 15.36
460 days
10450 days
4088
3468
1776
2507
days
days
days
days
1998 days
3777 days
3088 days
7357 days
11925 days
11412 days
653 days
1260 days
892 days
3925 days
4031 days
3195 days
11191 days
4091 days
4745 days
4946
4929
4915
7716
7531
days
days
days
days
days
6912 days
6810 days
Cosmos 375 fragments, 45 pieces, 21 have decayed
Cosmos 375 was launched on a two-revolution rendezvous with Cosmos 373. The fragmentation occurred in the vicinity of Cosmos 373 on 1970 Oct 30 at 06:00 UT
near 54ºN 23ºE. Cosmos 375 was part of test series begun with Cosmos 249.
D 1970-91 C
[04623]
2001 Mar 11
11090 days
D 1970-91 D
[04624]
2000 Jun 8
10814 days
D 1970-91 E
[04625]
2000 Nov 24
10983 days
D 1970-91 F
[04626]
1980 Feb 20
3400 days
D 1970-91 G
[04627]
1988 Nov 25
6601 days
1970-91 H
[04628]
2002 Dec 15.92
62.76
104.05
7329
496
1405
0.062
51
1970-91 J
[04629]
2002 Dec 15.93
62.86
110.85
7645
562
1971
0.092
215
2014 – version 1.13
RAE Table of Earth Satellites
Year of Launch 1970
Cospar ID
D
D
D
D
D
D
D
D
D
D
D
D
D
D
D
D
D
D
D
D
D
D
D
D
1970-91
1970-91
1970-91
1970-91
1970-91
1970-91
1970-91
1970-91
1970-91
1970-91
1970-91
1970-91
1970-91
1970-91
1970-91
1970-91
1970-91
1970-91
1970-91
1970-91
1970-91
1970-91
1970-91
1970-91
1970-91
1970-91
1970-91
1970-91
1970-91
1970-91
1970-91
1970-91
1970-91
1970-91
1970-91
1970-91
1970-91
1970-91
[Norad number]
K
L
M
N
P
Q
R
S
T
U
V
W
X
Y
Z
AA
AB
AC
AD
AE
AF
AG
AH
AJ
AK
AL
AM
AN
AP
AQ
AR
AS
AT
AU
AV
AW
AX
AY
[04633]
[04634]
[04635]
[04661]
[04662]
[04663]
[04664]
[04665]
[04712]
[04723]
[04724]
[04725]
[04726]
[04727]
[04728]
[04729]
[04730]
[04731]
[04826]
[04827]
[04828]
[04896]
[04940]
[04941]
[04942]
[05082]
[05083]
[05084]
[05089]
[05093]
[13775]
[14527]
[14838]
[18798]
[18866]
[19023]
[19949]
[19960]
Orbiting Frog Otolith 1 fragments,
D 1970-94 C
[04693]
D 1970-94 D
[04747]
D 1970-94 E
[04844]
Cosmos 381 fragments,
D 1970-102 C
1970-102 D
1970-102 E
2014 – version 1.13
Descent date
Lifetime
1984 Feb 21
4862 days
1995 Aug 30
1982 Apr 7
1988 Aug 24
1988 Aug 27
2001 Jul 7
1980
1978
1981
1981
1990
1980
1977
2001
1988
2005
1982
1976
1999
2000
1990
1989
1989
Nov
Nov
Feb
Aug
Mar
Nov
Sep
Aug
Aug
Jan
Nov
Dec
Oct
Sep
Aug
Nov
Jan
22
26
24 A
5
2
9
16
13
29
23
22 A
5
26
11
29
1
23
1989 Dec 27
(Revised 2002)
Extra Page 1970 - 12
Semi
major axis
(km)
Perigee
height
(km)
Apogee
height
(km)
Orbital
Argument
eccentricity of perigee
(deg)
7384
7632
519
570
1493
1937
0.066
0.090
14
313
98.28
108.45
105.10
101.18
104.52
7055
7534
7378
7193
7350
484
490
504
476
503
870
1821
1495
1154
1441
0.027
0.088
0.067
0.047
0.064
192
72
47
121
47
62.71
62.88
104.60
107.97
7354
7511
552
504
1400
1762
0.058
0.084
247
88
2002 Dec 22.11
2002 Dec 21.44
62.77
63.06
100.27
111.52
7150
7675
463
553
1080
2040
0.043
0.097
107
67
2002 Dec 15.89
62.79
96.20
6955
415
738
0.023
93
2002 Dec 19.71
62.69
108.90
7554
566
1786
0.081
278
2002 Dec 20.28
2002 Dec 21.48
62.61
62.89
105.05
110.23
7375
7616
509
520
1485
1956
0.066
0.094
129
94
2002 Dec 15.90
2002 Dec 16.06
74.02
74.03
103.78
104.05
7316
7329
926
935
950
966
0.002
0.002
20
21
Date of
orbital
determination
Orbital
Inclination
(deg)
Nodal
period
(min)
2002 Dec 15.63
2002 Dec 15.90
62.81
62.83
105.14
110.58
2002
2002
2002
2002
2002
16.50
15.95
15.74
16.06
15.99
62.72
62.53
62.78
62.75
62.78
2002 Dec 21.58
2002 Dec 22.31
9047 days
4177 days
6508 days
Dec
Dec
Dec
Dec
Dec
6511 days
11208 days
3645 days
2949 days
3770 days
3932 days
7063 days
3663 days
2513 days
11245 days
6513 days
12504 days
4406 days
2228 days
10588 days
10909 days
7243 days
6942 days
6660 days
6998 days
3 pieces, all have decayed
1970 Dec 18
39 days
1971 Jan 25
77 days
1971 Jan 21
73 days
4 pieces, 2 have decayed
[04840]
1992 Apr 23
[05225]
[08764]
7813 days
RAE Table of Earth Satellites
Year of Launch 1970
Cospar ID
D
[Norad number]
1970-102 F
Cosmos 382 fragments,
D 1970-103 D
D 1970-103 E
D 1970-103 F
1970-103 G
2014 – version 1.13
[09794]
Descent date
Lifetime
1998 Dec 22
10247 days
4 pieces, 3 have decayed
[05316]
1990 Nov 7
[05326]
1977 Jan 3
[06072]
1977 Jan 3
[12854]
Date of
orbital
determination
Orbital
Inclination
(deg)
Nodal
period
(min)
2002 Dec 17.59
50.34
134.35
(Revised 2002)
Extra Page 1970 - 13
Semi
major axis
(km)
Perigee
height
(km)
Apogee
height
(km)
Orbital
Argument
eccentricity of perigee
(deg)
918
3705
0.160
7280 days
2224 days
2224 days
8690
113