| Thumba |
home
topic index |
||
Type: Suborbital Launch Site. Operator: India. Country: India. Latitude: 8.53144 deg. Longitude: 76.86899 deg. Sounding rocket launch location known to have been used for 1385 launches from 1963 to 2004, reaching up to 400 kilometers altitude. Launch Pads
General / Launch Complex Unknown Chronology 1963 November 21 - 12:55 GMT - Launch Vehicle: Apache. Nike Apache NASA 14.128IA ISRO 10.01 (Na) Aeronomy mission Agency: NASA. Apogee: 208 km (129 mi). 1964 January 8 - 13:15 GMT - Launch Vehicle: Apache. Nike Apache NASA 14.129IA ISRO 10.02? (Na) Aeronomy mission Agency: NASA. Apogee: 187 km (116 mi). 1964 January 12 - 00:26 GMT - Launch Vehicle: Apache. Nike Apache NASA 14.130IA ISRO 10.03? (Na) Aeronomy mission Agency: NASA. Apogee: 187 km (116 mi). 1964 January 25 - 05:30 GMT - Launch Vehicle: Apache. Nike Apache NASA 14.79UE UNH64-1 ISRO 20.01? E'jet Magnetospheric mission Agency: NASA. Apogee: 164 km (101 mi). 1964 January 27 - 04:30 GMT - Launch Vehicle: Apache. Nike Apache NASA 14.80UE UNH64-2 ISRO 20.02? E'jet Magnetospheric mission Agency: NASA. Apogee: 164 km (101 mi). 1964 January 29 - 10:00 GMT - Launch Vehicle: Apache. Nike Apache NASA 14.81UE UNH64-3 ISRO 20.03? E'jet Magnetospheric mission Agency: NASA. Apogee: 167 km (103 mi). 1964 January 31 - 13:30 GMT - Launch Vehicle: Apache. Nike Apache NASA 14.82UE UNH64-4 ISRO 20.04? E'jet Magnetospheric mission Agency: NASA. Apogee: 167 km (103 mi). 1964 July 14 - 06:54 GMT - Launch Vehicle: Loki. Judi-Dart TERLS-8 ISRO 11.01 Aeronomy mission Agency: ISRO. Apogee: 76 km (47 mi). 1964 July 15 - 09:55 GMT - Launch Vehicle: Loki. Judi-Dart TERLS-9 ISRO 11.02 Aeronomy mission Agency: ISRO. Apogee: 76 km (47 mi). 1964 July 16 - 09:10 GMT - Launch Vehicle: Loki. Judi-Dart TERLS-10 ISRO 11.03 Aeronomy mission Agency: ISRO. Apogee: 76 km (47 mi). 1964 August 19 - 06:01 GMT - Launch Vehicle: Loki. Judi-Dart TERLS-11 ISRO 11.04 Aeronomy mission Agency: ISRO. Apogee: 78 km (48 mi). 1964 November 6 - 00:08 GMT - Launch Vehicle: Apache. Nike Apache NASA 14.131IA ISRO 10.04? TERLS-12 Aeronomy sodium release mission Agency: NASA. Apogee: 192 km (119 mi). 1964 November 9 - 12:54 GMT - Launch Vehicle: Apache. Nike Apache NASA 14.204IA ISRO 10.05 / TERLS-13? Aeronomy sodium release mission Agency: NASA. Apogee: 192 km (119 mi). 1964 November 10 - 00:05 GMT - Launch Vehicle: Apache. Nike Apache NASA 14.205IA ISRO 10.06 / TERLS-14? Aeronomy sodium release mission Agency: NASA. Apogee: 192 km (119 mi). 1964 December 5 - 06:55 GMT - Launch Vehicle: Loki. Judi-Dart TERLS-15 ISRO 11.05 Aeronomy mission Agency: ISRO. Apogee: 77 km (47 mi). 1964 December 15 - 06:30 GMT - Launch Vehicle: Loki. Judi-Dart TERLS-16 ISRO 11.06 Aeronomy mission Agency: ISRO. Apogee: 77 km (47 mi). 1964 December 16 - 07:38 GMT - Launch Vehicle: Loki. Judi-Dart TERLS-17 ISRO 11.07 Aeronomy mission Agency: ISRO. Apogee: 77 km (47 mi). 1965 January 12 - 10:59 GMT - Launch Vehicle: Loki. Judi-Dart TERLS-18 ISRO 11.08 Aeronomy mission Agency: ISRO. Apogee: 77 km (47 mi). 1965 January 13 - 10:15 GMT - Launch Vehicle: Loki. Judi-Dart TERLS-19 ISRO 11.09 Aeronomy mission Agency: ISRO. Apogee: 77 km (47 mi). 1965 February 3 - 07:39 GMT - Launch Vehicle: Loki. Judi-Dart TERLS-20 ISRO 11.10 Aeronomy mission Agency: ISRO. Apogee: 77 km (47 mi). 1965 March 17 - 06:55 GMT - Launch Vehicle: Loki. Judi-Dart TERLS-21 ISRO 11.11 Aeronomy mission Agency: ISRO. Apogee: 77 km (47 mi). 1965 April 28 - 23:57 GMT - Launch Vehicle: Belier. Centaure C99 TERLS-22? ISRO 15.02 Aeronomy / ionosphere mission Agency: ISRO. Apogee: 150 km (90 mi). 1965 May 1 - 23:43 GMT - Launch Vehicle: Belier. Centaure C100 TERLS-23? ISRO 15.01 Ionosphere mission Agency: ISRO. Apogee: 140 km (80 mi). 1965 May 19 - 07:04 GMT - Launch Vehicle: Loki. Judi-Dart TERLS-24? ISRO 11.12 Aeronomy mission Agency: ISRO. Apogee: 77 km (47 mi). 1965 June 16 - 07:04 GMT - Launch Vehicle: Loki. Judi-Dart TERLS-25 ISRO 11.13 Aeronomy mission Agency: ISRO. Apogee: 77 km (47 mi). 1965 July 21 - 02:50 GMT - Launch Vehicle: Loki. Judi-Dart TERLS-26 ISRO 11.14 Aeronomy mission Agency: ISRO. Apogee: 77 km (47 mi). 1965 August 18 - 07:10 GMT - Launch Vehicle: Loki. Judi-Dart TERLS-27 ISRO 11.15 Aeronomy mission Agency: ISRO. Apogee: 77 km (47 mi). 1965 September 15 - 09:31 GMT - Launch Vehicle: Loki. Judi-Dart TERLS-28 ISRO 11.16 Aeronomy mission Agency: ISRO. Apogee: 77 km (47 mi). 1965 October 20 - 07:05 GMT - Launch Vehicle: Loki. Judi-Dart TERLS-29 ISRO 11.17 Aeronomy mission Agency: ISRO. Apogee: 77 km (47 mi). 1965 November 17 - 08:36 GMT - Launch Vehicle: Loki. Judi-Dart TERLS-30 ISRO 11.18 Aeronomy mission Agency: ISRO. Apogee: 77 km (47 mi). 1965 November 23 - 02:27 GMT - Launch Vehicle: Loki. Judi-Dart TERLS-31 ISRO 19.01 Aeronomy mission Agency: ISRO. Apogee: 69 km (42 mi). 1965 December 15 - 07:35 GMT - Launch Vehicle: Loki. Judi-Dart TERLS-32 ISRO 11.20 Aeronomy mission Agency: ISRO. Apogee: 77 km (47 mi). 1965 December 17 - 06:36 GMT - Launch Vehicle: Loki. Judi-Dart TERLS-33 ISRO 11.21 Aeronomy mission Agency: ISRO. Apogee: 75 km (46 mi). 1965 December 18 - 06:47 GMT - Launch Vehicle: Loki. Judi-Dart TERLS-34 ISRO 11.22 Aeronomy mission Agency: ISRO. Apogee: 75 km (46 mi). 1966 January 8 - 13:11 GMT - Launch Vehicle: Belier. Centaure C103 TERLS-35 ISRO 15.03 Aeronomy / ionosphere mission Agency: ISRO. Apogee: 150 km (90 mi). 1966 January 19 - 09:30 GMT - Launch Vehicle: Loki. Judi-Dart TERLS-36 ISRO 11.23 Aeronomy mission Agency: ISRO. Apogee: 67 km (41 mi). 1966 February 16 - 03:30 GMT - Launch Vehicle: Loki. Judi-Dart TERLS-37 ISRO 11.24 Aeronomy mission Agency: ISRO. Apogee: 67 km (41 mi). 1966 March 16 - 12:10 GMT - Launch Vehicle: Loki. Judi-Dart TERLS-38 ISRO 11.25 Aeronomy mission Agency: ISRO. Apogee: 62 km (38 mi). 1966 March 24 - 13:30 GMT - Launch Vehicle: Apache. Nike Apache NASA 14.257IA ISRO 10.07 TERLS-39 Aeronomy mission Agency: ISRO. Apogee: 201 km (124 mi). 1966 March 24 - 16:45 GMT - Launch Vehicle: Belier. Centaure C101 TERLS-40 ISRO 15.04 Aeronomy mission Agency: ISRO. Apogee: 163 km (101 mi). 1966 March 24 - 21:00 GMT - Launch Vehicle: Belier. Centaure C102 TERLS-41 ISRO 15.05 Aeronomy mission Agency: ISRO. Apogee: 159 km (98 mi). 1966 March 25 - 00:19 GMT - Launch Vehicle: Apache. Nike Apache NASA 14.258IA ISRO 10.08 TERLS-42 Aeronomy mission Agency: ISRO. Apogee: 201 km (124 mi). 1966 April 13 - 07:30 GMT - Launch Vehicle: Loki. Judi-Dart TERLS-43 ISRO 11.26 Aeronomy mission Agency: ISRO. Apogee: 69 km (42 mi). 1966 July 7 - 08:15 GMT - Launch Vehicle: Apache. Nike Apache NASA 14.59IE ISRO 20.05 / TERLS-44 Plasma mission Agency: NASA. Apogee: 178 km (110 mi). 1966 July 13 - 06:20 GMT - Launch Vehicle: Loki. Judi-Dart TERLS-45 ISRO 11.27 Aeronomy mission Agency: ISRO. Apogee: 45 km (27 mi). 1966 August 7 - 08:45 GMT - Launch Vehicle: Apache. ISRO 20.05 TERLS-46? Ionosphere mission Agency: ISRO. Apogee: 175 km (108 mi). 1967 March 6 - 13:27 GMT - Launch Vehicle: Apache. Nike Apache NASA 14.161IA ISRO 10.09 (Release) Aeronomy mission Agency: NASA. Apogee: 178 km (110 mi). 1967 March 9 - 13:27 GMT - Launch Vehicle: Apache. Nike Apache NASA 14.162IA ISRO 10.10 Aeronomy mission Agency: NASA. Apogee: 184 km (114 mi). 1967 March 12 - 13:27 GMT - Launch Vehicle: Apache. Nike Apache NASA 14.163IA-II ISRO 10.11 Ionosphere mission Agency: NASA. Apogee: 168 km (104 mi). 1967 March 12 - 17:00 GMT - Launch Vehicle: Apache. Nike Apache NASA 14.206IA ISRO 10.12 Ionosphere / aeronomy / chemica mission Agency: NASA. Apogee: 155 km (96 mi). 1967 March 13 - 00:14 GMT - Launch Vehicle: Apache. Nike Apache NASA 14.267IA ISRO 10.14 Ionosphere / aeronomy / chemica mission Agency: NASA. Apogee: 155 km (96 mi). 1967 April 19 - 06:14 GMT - Launch Vehicle: Belier. Centaure C87 ISRO 45.01 Ionosphere mission Agency: ISRO. Apogee: 128 km (79 mi). 1967 November 20 - 03:00 GMT - Launch Vehicle: RH. RH-75 1 TERLS-54 test Agency: ISRO. Apogee: 9.00 km (5.50 mi). First RH-75 launch. 1967 November 20 - 04:00 GMT - Launch Vehicle: RH. RH-75 2 Test mission Agency: ISRO. Apogee: 9.00 km (5.50 mi). 1967 November 20 - 05:15 GMT - Launch Vehicle: Loki. Judi-Dart TERLS-53 ISRO 11.28 Aeronomy mission Agency: ISRO. Apogee: 53 km (32 mi). 1967 December 1 - Launch Vehicle: RH. RH-75 3 Test mission Agency: ISRO. Apogee: 9.00 km (5.50 mi). 1967 December 20 - 09:39 GMT - Launch Vehicle: Loki. Judi-Dart TERLS-55 ISRO 11.29 Aeronomy mission Agency: ISRO. Apogee: 55 km (34 mi). 1968 January 1 - Launch Vehicle: RH. RH-75 4? Test mission Agency: ISRO. Apogee: 9.00 km (5.50 mi). 1968 January 1 - Launch Vehicle: RH. RH-75 5? Test mission Agency: ISRO. Apogee: 9.00 km (5.50 mi). 1968 January 1 - Launch Vehicle: RH. RH-75 6? Test mission Agency: ISRO. Apogee: 9.00 km (5.50 mi). 1968 February 1 - Launch Vehicle: RH. RH-75 8 Test mission Agency: ISRO. Apogee: 9.00 km (5.50 mi). 1968 February 1 - Launch Vehicle: RH. RH-75 7 Test mission Agency: ISRO. Apogee: 9.00 km (5.50 mi). 1968 February 2 - Launch Vehicle: Loki. Aeronomy mission Agency: ISRO. Apogee: 70 km (43 mi). 1968 February 2 - 13:26 GMT - Launch Vehicle: Apache. Nike Apache NASA 14.259IA INCOSPAR 10.13 ISRO Aeronomy / ionosphere mission Agency: ISRO. Apogee: 191 km (118 mi). 1968 February 2 - 13:40 GMT - Launch Vehicle: Belier. Centaure C90 ISRO 15.06 Aeronomy mission Agency: ISRO. Apogee: 159 km (98 mi). 1968 February 21 - 19:40 GMT - Launch Vehicle: Belier. ISRO 25.02 Aeronomy mission Agency: ISRO. Apogee: 136 km (84 mi). 1968 February 22 - 11:25 GMT - Launch Vehicle: Belier. Centaure C89? ISRO 25.01 Aeronomy mission Agency: ISRO. Apogee: 153 km (95 mi). 1968 February 22 - 11:55 GMT - Launch Vehicle: Belier. Centaure C88 Aeronomy mission Agency: ISRO. Apogee: 154 km (95 mi). 1968 March 8 - 06:35 GMT - Launch Vehicle: Arcas. Boosted Arcas NASA 15.58UE ISRO 12.01 BRAHMA-I Plasma mission Agency: NASA. Apogee: 83 km (51 mi). 1968 March 8 - 12:40 GMT - Launch Vehicle: Arcas. Boosted Arcas NASA 15.59UE ISRO 12.02 BRAHMA-II Plasma mission Agency: NASA. Apogee: 94 km (58 mi). 1968 March 28 - 01:32 GMT - Launch Vehicle: Apache. Nike Apache NASA 14.375IE-II ISRO 10.15 Ionosphere mission Agency: ISRO. Apogee: 211 km (131 mi). 1968 March 30 - 13:25 GMT - Launch Vehicle: Apache. Nike Apache NASA 14.376IE-II ISRO 10.16 Ionosphere mission Agency: ISRO. Apogee: 211 km (131 mi). 1968 March 31 - 00:07 GMT - Launch Vehicle: Apache. Nike Apache NASA 14.378IE ISRO 10.18 Ionosphere mission Agency: ISRO. Apogee: 211 km (131 mi). 1968 March 31 - 12:15 GMT - Launch Vehicle: Apache. Nike Apache NASA 14.377IE-II ISRO 10.17 Ionosphere mission Agency: ISRO. Apogee: 169 km (105 mi). 1968 April 22 - 15:53 GMT - Launch Vehicle: Apache. Nike Apache NASA 14.241IG ISRO 40.01 X-ray astronomy mission Agency: ISRO. Apogee: 159 km (98 mi). 1968 April 24 - 15:44 GMT - Launch Vehicle: Apache. Nike Apache NASA 14.260IG ISRO 40.02 X-ray astronomy mission Agency: ISRO. Apogee: 159 km (98 mi). 1968 August 29 - 05:38 GMT - Launch Vehicle: Apache. Nike Apache NASA 14.191 ISRO 20.06 Ionosphere mission Agency: NASA. Apogee: 170 km (100 mi). 1968 August 29 - 08:45 GMT - Launch Vehicle: Apache. Nike Apache NASA 14.192 ISRO 20.07 Ionosphere mission Agency: NASA. Apogee: 170 km (100 mi). 1968 August 29 - 17:30 GMT - Launch Vehicle: Apache. Nike Apache NASA 14.193 ISRO 20.08 Ionosphere mission Agency: NASA. Apogee: 168 km (104 mi). 1968 September 16 - Launch Vehicle: RH. Accelerometer test Agency: ISRO. Apogee: 9.00 km (5.50 mi). 1968 November 3 - 03:19 GMT - Launch Vehicle: Belier. ISRO 35.01 X-ray astronomy mission Agency: ISRO. Apogee: 159 km (98 mi). 1968 November 7 - 03:05 GMT - Launch Vehicle: Apache. Nike Apache NASA 14.261IG ISRO 40.03 X-ray astronomy mission Agency: NASA. Apogee: 150 km (90 mi). 1969 February 26 - 10:00 GMT - Launch Vehicle: Belier. Centaure ISRO-45.002 ISRO 45.02 Ionosphere mission Agency: ISRO. Apogee: 145 km (90 mi). 1969 April 26 - 17:00 GMT - Launch Vehicle: Apache. Nike Apache NASA 14.403IG ISRO 40.04 X-ray astronomy mission Agency: NASA. Apogee: 144 km (89 mi). 1969 April 28 - 17:04 GMT - Launch Vehicle: Apache. Nike Apache NASA 14.404IG ISRO 40.05 X-ray astronomy mission Agency: NASA. Apogee: 148 km (91 mi). 1969 June 11 - 05:20 GMT - Launch Vehicle: Loki. Judi-Dart TERLS-110 ISRO 11.30 Aeronomy mission Agency: ISRO. Apogee: 65 km (40 mi). 1969 June 25 - 06:12 GMT - Launch Vehicle: Loki. Judi-Dart TERLS-115 ISRO 11.31 Aeronomy mission Agency: ISRO. Apogee: 64 km (39 mi). 1969 July 16 - 05:30 GMT - Launch Vehicle: Loki. Judi-Dart TERLS-116 ISRO 11.32 Aeronomy mission Agency: ISRO. Apogee: 64 km (39 mi). 1969 July 23 - 05:50 GMT - Launch Vehicle: Loki. Judi-Dart TERLS-117 ISRO 11.33 Aeronomy mission Agency: ISRO. Apogee: 64 km (39 mi). 1969 July 30 - 05:30 GMT - Launch Vehicle: Loki. Judi-Dart ISRO 11.34 ISRO 11.34 Aeronomy mission Agency: ISRO. Apogee: 29 km (18 mi). 1969 August 6 - 05:50 GMT - Launch Vehicle: Loki. Judi-Dart ISRO 11.35 ISRO 11.35 Aeronomy mission Agency: ISRO. Apogee: 64 km (39 mi). 1969 August 20 - 10:57 GMT - Launch Vehicle: Loki. Judi-Dart ISRO 11.36 ISRO 11.36 Aeronomy mission Agency: ISRO. Apogee: 64 km (39 mi). 1969 September 20 - 20:00 GMT - Launch Vehicle: Belier. LV Model: Dragon 1 . Dragon D-39 ISRO 26.01 Ionosphere mission Agency: ISRO. Apogee: 400 km (240 mi). 1969 December 7 - 00:35 GMT - Launch Vehicle: Belier. Centaure 2A ISRO-45.003 ISRO 45.03 Test / ionosphere / x-ray astronomy mission Agency: ISRO. Apogee: 123 km (76 mi). 1970 - Launch Vehicle: RH. First Flight test Agency: ISRO. Apogee: 40 km (24 mi). 1970 - Launch Vehicle: RH. First Flight test Agency: ISRO. Apogee: 11 km (6 mi). 1970 January 2 - 06:42 GMT - Launch Vehicle: Apache. Nike Apache NASA 14.240II ISRO 30.01 Ionosphere mission Agency: NASA. Apogee: 125 km (77 mi). 1970 February 18 - 09:35 GMT - Launch Vehicle: Skua. LV Model: Skua 1 . Skua Su13T/C ISRO 16.01 Ionosphere mission Agency: SRC. Apogee: 92 km (57 mi). 1970 March 6 - 13:45 GMT - Launch Vehicle: Skua. LV Model: Skua 1 . Skua ISRO 16.02 ISRO 16.02 Aeronomy mission Agency: ISRO. Apogee: 61 km (37 mi). 1970 March 8 - 13:45 GMT - Launch Vehicle: Skua. LV Model: Skua 1 . Skua ISRO-16.003 ISRO 16.03 TERLS-155 Aeronomy mission Agency: ISRO. Apogee: 58 km (36 mi). 1970 March 9 - 08:25 GMT - Launch Vehicle: Tomahawk Sandia. Nike Tomahawk NASA 18.99GI ISRO 17.03 Ionosphere mission Agency: NASA. Apogee: 264 km (164 mi). 1970 March 9 - 14:30 GMT - Launch Vehicle: Tomahawk Sandia. Nike Tomahawk NASA 18.97GI ISRO 17.01 Ionosphere mission Agency: NASA. Apogee: 298 km (185 mi). 1970 March 9 - 19:38 GMT - Launch Vehicle: Tomahawk Sandia. Nike Tomahawk NASA 18.98GI ISRO 17.02? Ionosphere mission Agency: NASA. Apogee: 296 km (183 mi). 1970 March 10 - 14:15 GMT - Launch Vehicle: Skua. LV Model: Skua 1 . Skua ISRO-16.004 ISRO 16.04 TERLS-159 Aeronomy mission Agency: ISRO. Apogee: 60 km (37 mi). 1970 March 12 - 13:45 GMT - Launch Vehicle: Skua. LV Model: Skua 1 . Skua ISRO-16.005 ISRO 16.05 TERLS-160 Aeronomy mission Agency: ISRO. Apogee: 66 km (41 mi). 1970 March 14 - 13:05 GMT - Launch Vehicle: Skua. LV Model: Skua 1 . Skua ISRO-16.006 ISRO 16.06 TERLS-161 Aeronomy mission Agency: ISRO. Apogee: 63 km (39 mi). 1970 March 16 - 13:45 GMT - Launch Vehicle: Skua. LV Model: Skua 1 . Skua ISRO-16.007 ISRO 16.07 TERLS-162 Aeronomy mission Agency: ISRO. Apogee: 62 km (38 mi). 1970 March 16 - 23:50 GMT - Launch Vehicle: Skua. LV Model: Skua 1 . Skua ISRO-16.008 ISRO 16.08 TERLS-163 Aeronomy mission Agency: ISRO. Apogee: 62 km (38 mi). 1970 March 18 - 13:45 GMT - Launch Vehicle: Skua. LV Model: Skua 1 . Skua ISRO-16.009 ISRO 16.09 TERLS-169 Aeronomy mission Agency: ISRO. Apogee: 62 km (38 mi). 1970 March 19 - 03:19 GMT - Launch Vehicle: Apache. Nike Apache NASA 14.425GI ISRO 10.33 / 17.04 Ionosphere mission Agency: NASA. Apogee: 200 km (120 mi). 1970 March 19 - 05:09 GMT - Launch Vehicle: Apache. Nike Apache NASA 14.424GI ISRO 10.34 / 17.05 Ionosphere mission Agency: NASA. Apogee: 97 km (60 mi). 1970 March 19 - 10:01 GMT - Launch Vehicle: Apache. Nike Apache NASA 14.372GI ISRO 10.35 / 17.06 Ionosphere mission Agency: NASA. Apogee: 196 km (121 mi). 1970 March 20 - 13:45 GMT - Launch Vehicle: Skua. LV Model: Skua 1 . Skua ISRO-16.010 ISRO 16.10 TERLS-173 Aeronomy mission Agency: ISRO. Apogee: 68 km (42 mi). 1970 March 22 - 13:35 GMT - Launch Vehicle: Skua. LV Model: Skua 1 . Skua ISRO-16.011 ISRO 16.11 TERLS-174 Aeronomy mission Agency: ISRO. Apogee: 64 km (39 mi). 1970 March 27 - 05:25 GMT - Launch Vehicle: Apache. Nike Apache NASA 14.405IE/II ISRO 10.36 Plasma / ionosphere mission Agency: NASA. Apogee: 195 km (121 mi). 1970 March 27 - 07:00 GMT - Launch Vehicle: Arcas. Arcas NASA 15.54GI ISRO-12.03 Ionosphere mission Agency: NASA. Apogee: 68 km (42 mi). 1970 March 27 - 12:42 GMT - Launch Vehicle: Arcas. Boosted Arcas 2 NASA 15.63UE ISRO-12.04 Plasma mission Agency: NASA. Apogee: 93 km (57 mi). 1970 March 27 - 13:06 GMT - Launch Vehicle: Arcas. Boosted Arcas 2 NASA 15.64UE ISRO-12.05 Plasma mission Agency: NASA. Apogee: 103 km (64 mi). 1970 March 27 - 13:30 GMT - Launch Vehicle: Arcas. Boosted Arcas 2 NASA 15.65UE ISRO-12.06 Plasma mission Agency: NASA. Apogee: 97 km (60 mi). 1970 April 15 - 10:05 GMT - Launch Vehicle: Skua. LV Model: Skua 1 . Skua Su15T/C ISRO-16.13 Ionosphere mission Agency: SRC. Apogee: 93 km (57 mi). 1970 April 16 - 01:50 GMT - Launch Vehicle: Skua. LV Model: Skua 1 . Skua Su14T/C ISRO-16.12 Ionosphere mission Agency: SRC. Apogee: 91 km (56 mi). 1970 December 9 - 17:45 GMT - Launch Vehicle: M-100. ISRO-8.001 Apogee: 91 km (56 mi). 1970 December 16 - 17:36 GMT - Launch Vehicle: M-100. ISRO-8.002 Apogee: 93 km (57 mi). 1970 December 23 - 17:30 GMT - Launch Vehicle: M-100. ISRO-8.003 Apogee: 93 km (57 mi). 1970 December 30 - 17:35 GMT - Launch Vehicle: M-100. ISRO-8.004 Apogee: 94 km (58 mi). 1971 January 6 - 17:30 GMT - Launch Vehicle: M-100. ISRO-8.005 Apogee: 89 km (55 mi). 1971 January 7 - 00:27 GMT - Launch Vehicle: Belier. Centaure 2A ISRO 5.12 FAILURE: Failure. ISRO 5.12 Recovery Test / aeronomy mission Agency: ISRO. Apogee: 10 km (6 mi). 1971 January 13 - 17:35 GMT - Launch Vehicle: M-100. ISRO-8.006 Apogee: 94 km (58 mi). 1971 January 20 - 04:30 GMT - Launch Vehicle: M-100. ISRO-8.007 Apogee: 91 km (56 mi). 1971 January 20 - 17:30 GMT - Launch Vehicle: M-100. ISRO-8.008 Apogee: 90 km (55 mi). 1971 January 28 - 05:10 GMT - Launch Vehicle: Apache. Nike Apache NASA 14.409II ISRO 10.37 Ionosphere mission Agency: NASA. Apogee: 163 km (101 mi). 1971 January 28 - 05:40 GMT - Launch Vehicle: Apache. Nike Apache NASA 14.410II ISRO 10.38 Ionosphere mission Agency: NASA. Apogee: 189 km (117 mi). 1971 January 30 - 05:22 GMT - Launch Vehicle: M-100. ISRO-8.009 Apogee: 89 km (55 mi). 1971 February 3 - 19:05 GMT - Launch Vehicle: M-100. ISRO-8.010 Apogee: 91 km (56 mi). 1971 February 10 - 18:00 GMT - Launch Vehicle: M-100. ISRO-8.011 Apogee: 91 km (56 mi). 1971 February 17 - 17:30 GMT - Launch Vehicle: M-100. ISRO-8.012 Apogee: 84 km (52 mi). 1971 February 24 - 17:30 GMT - Launch Vehicle: M-100. ISRO-8.013 Apogee: 91 km (56 mi). 1971 March 3 - 18:00 GMT - Launch Vehicle: M-100. ISRO-8.014 Apogee: 90 km (55 mi). 1971 March 10 - 17:30 GMT - Launch Vehicle: M-100. ISRO-8.015 Apogee: 90 km (55 mi). 1971 March 17 - 16:30 GMT - Launch Vehicle: M-100. ISRO-8.016 Apogee: 92 km (57 mi). 1971 March 24 - 16:50 GMT - Launch Vehicle: M-100. ISRO-8.017 Apogee: 89 km (55 mi). 1971 March 31 - 16:30 GMT - Launch Vehicle: M-100. ISRO-8.018 Apogee: 89 km (55 mi). 1971 April 5 - 13:57 GMT - Launch Vehicle: M-100. ISRO-8.019 Apogee: 88 km (54 mi). 1971 April 5 - 14:02 GMT - Launch Vehicle: M-100. ISRO-8.020 Apogee: 90 km (55 mi). 1971 April 19 - 13:25 GMT - Launch Vehicle: Apache. Nike Apache NASA 14.406IA ISRO 10.41 Aeronomy mission Agency: NASA. Apogee: 198 km (123 mi). 1971 April 25 - 06:00 GMT - Launch Vehicle: Apache. Nike Apache NASA 14.407II/IE ISRO 10.40 Ionosphere / plasma mission Agency: NASA. Apogee: 160 km (90 mi). 1971 April 25 - 13:25 GMT - Launch Vehicle: Apache. Nike Apache NASA 14.408IA ISRO 10.39 Aeronomy mission Agency: NASA. Apogee: 100 km (60 mi). 1971 April 30 - 06:08 GMT - Launch Vehicle: Apache. Nike Apache NASA 14.411II ISRO 10.42 Ionosphere mission Agency: NASA. Apogee: 171 km (106 mi). 1971 May 19 - 14:35 GMT - Launch Vehicle: M-100. ISRO-8.21 Apogee: 90 km (55 mi). 1971 May 26 - 14:40 GMT - Launch Vehicle: M-100. ISRO-8.22 Apogee: 92 km (57 mi). 1971 June 2 - 14:40 GMT - Launch Vehicle: M-100. ISRO-8.23 Apogee: 89 km (55 mi). 1971 June 9 - 14:40 GMT - Launch Vehicle: M-100. ISRO-8.24 Apogee: 85 km (52 mi). 1971 June 16 - 14:30 GMT - Launch Vehicle: M-100. ISRO-8.25 Apogee: 91 km (56 mi). 1971 June 23 - 14:45 GMT - Launch Vehicle: M-100. ISRO-8.26 Apogee: 91 km (56 mi). 1971 June 30 - 16:06 GMT - Launch Vehicle: M-100. ISRO-8.27 Apogee: 88 km (54 mi). 1971 July 7 - 14:30 GMT - Launch Vehicle: M-100. ISRO-8.28 Apogee: 94 km (58 mi). 1971 July 14 - 14:34 GMT - Launch Vehicle: M-100. ISRO-8.29 Apogee: 89 km (55 mi). 1971 July 21 - 14:30 GMT - Launch Vehicle: M-100. ISRO-8.30 Apogee: 92 km (57 mi). 1971 July 28 - 14:37 GMT - Launch Vehicle: M-100. ISRO-8.31 Apogee: 91 km (56 mi). 1971 August 4 - 14:30 GMT - Launch Vehicle: M-100. ISRO-8.32 Apogee: 91 km (56 mi). 1971 August 4 - 15:00 GMT - Launch Vehicle: M-100. Apogee: 91 km (56 mi). 1971 August 11 - 14:33 GMT - Launch Vehicle: M-100. ISRO-8.33 Apogee: 87 km (54 mi). 1971 August 11 - 15:00 GMT - Launch Vehicle: M-100. Apogee: 90 km (55 mi). 1971 August 18 - 14:30 GMT - Launch Vehicle: M-100. ISRO-8.34 Apogee: 92 km (57 mi). 1971 August 25 - 14:30 GMT - Launch Vehicle: M-100. ISRO-8.35 Apogee: 90 km (55 mi). 1971 September 1 - 14:30 GMT - Launch Vehicle: M-100. M-100 TERLS-345 ISRO-8.36 Apogee: 90 km (55 mi). 1971 September 8 - 14:30 GMT - Launch Vehicle: M-100. M-100 TERLS-346? ISRO-8.37 Apogee: 90 km (55 mi). 1971 September 15 - 14:05 GMT - Launch Vehicle: M-100. M-100 TERLS-347 ISRO-8.38 Apogee: 91 km (56 mi). 1971 September 22 - 14:30 GMT - Launch Vehicle: M-100. ISRO-8.39 Apogee: 90 km (55 mi). 1971 September 29 - 14:30 GMT - Launch Vehicle: M-100. ISRO-8.40 Apogee: 88 km (54 mi). 1971 October 6 - 14:30 GMT - Launch Vehicle: M-100. M-100 TERLS-363 ISRO-8.41 Apogee: 90 km (55 mi). 1971 October 13 - 14:31 GMT - Launch Vehicle: M-100. ISRO-8.42 Apogee: 87 km (54 mi). 1971 October 20 - 14:30 GMT - Launch Vehicle: M-100. ISRO-8.43 Apogee: 80 km (49 mi). 1971 October 27 - 16:20 GMT - Launch Vehicle: M-100. ISRO-8.44 Apogee: 89 km (55 mi). 1971 November 3 - 14:30 GMT - Launch Vehicle: M-100. ISRO-8.45 Apogee: 90 km (55 mi). 1971 November 10 - 14:30 GMT - Launch Vehicle: M-100. ISRO-8.46 Apogee: 87 km (54 mi). 1971 November 17 - 14:30 GMT - Launch Vehicle: M-100. Apogee: 92 km (57 mi). 1971 November 17 - 14:30 GMT - Launch Vehicle: M-100. ISRO-8.47 Apogee: 90 km (55 mi). 1971 November 24 - 14:30 GMT - Launch Vehicle: M-100. ISRO-8.48 Apogee: 90 km (55 mi). 1971 December 1 - 14:30 GMT - Launch Vehicle: M-100. ISRO-8.49 Apogee: 90 km (55 mi). 1971 December 8 - 14:30 GMT - Launch Vehicle: M-100. M-100 TERLS-390 ISRO-8.50 Apogee: 87 km (54 mi). 1971 December 15 - 15:00 GMT - Launch Vehicle: M-100. Apogee: 87 km (54 mi). 1971 December 15 - 15:00 GMT - Launch Vehicle: M-100. M-100 TERLS-391 ISRO-8.51 Apogee: 87 km (54 mi). 1971 December 22 - 15:00 GMT - Launch Vehicle: M-100. Apogee: 90 km (55 mi). 1971 December 22 - 15:00 GMT - Launch Vehicle: M-100. M-100 TERLS-396 ISRO-8.52 Apogee: 86 km (53 mi). 1971 December 29 - 14:30 GMT - Launch Vehicle: M-100. M-100 TERLS-397 ISRO-8.53 Apogee: 92 km (57 mi). 1971 December 29 - 15:00 GMT - Launch Vehicle: M-100. Apogee: 87 km (54 mi). 1972 January 4 - 13:14 GMT - Launch Vehicle: Petrel. LV Model: Petrel 1 . Petrel P78T/C ISRO 18.01 Ionosphere mission Agency: SRC. Apogee: 167 km (103 mi). 1972 January 5 - 13:14 GMT - Launch Vehicle: Skua. LV Model: Skua 1 . Skua SK30T/C FAILURE: Failure. ISRO-16.14 Ionosphere / barium release mission Agency: SRC. Apogee: 2.00 km (1.20 mi). 1972 January 5 - 14:33 GMT - Launch Vehicle: M-100. M-100 TERLS-400 ISRO-8.54 Apogee: 87 km (54 mi). 1972 January 6 - 13:14 GMT - Launch Vehicle: Petrel. LV Model: Petrel 1 . Petrel P95T/C ISRO 18.02 Ionosphere mission Agency: SRC. Apogee: 126 km (78 mi). 1972 January 7 - 13:11 GMT - Launch Vehicle: Petrel. LV Model: Petrel 1 . Petrel P77T/C ISRO 18.03 Ionosphere mission Agency: SRC. Apogee: 166 km (103 mi). 1972 January 12 - 14:30 GMT - Launch Vehicle: M-100. M-100 TERLS-403 ISRO-8.55 Apogee: 89 km (55 mi). 1972 January 12 - 15:00 GMT - Launch Vehicle: M-100. Apogee: 89 km (55 mi). 1972 January 14 - 18:13 GMT - Launch Vehicle: Petrel. LV Model: Petrel 1 . Petrel P89T/C ISRO 18.04 Ionosphere mission Agency: SRC. Apogee: 128 km (79 mi). 1972 January 18 - 00:37 GMT - Launch Vehicle: Skua. LV Model: Skua 1 . Skua SK31T/C ISRO-16.15 Ionosphere / barium release mission Agency: SRC. Apogee: 40 km (24 mi). 1972 January 18 - 05:35 GMT - Launch Vehicle: Petrel. LV Model: Petrel 1 . Petrel P88T/C FAILURE: Failure. ISRO 18.05 Ionosphere mission Agency: SRC. Apogee: 23 km (14 mi). 1972 January 19 - 14:31 GMT - Launch Vehicle: M-100. M-100 TERLS-407 ISRO-8.56 Apogee: 91 km (56 mi). 1972 January 26 - 15:00 GMT - Launch Vehicle: M-100. M-100 TERLS-408 ISRO-8.57 Apogee: 89 km (55 mi). 1972 January 26 - 16:55 GMT - Launch Vehicle: M-100. Apogee: 89 km (55 mi). 1972 January 31 - 13:22 GMT - Launch Vehicle: Skua. Skua 2 SK32T/C ISRO-16.16 Ionosphere / barium release mission Agency: SRC. Apogee: 79 km (49 mi). 1972 February 2 - 05:30 GMT - Launch Vehicle: Petrel. LV Model: Petrel 1 . Petrel P110T/C ISRO 18.06 Ionosphere mission Agency: SRC. Apogee: 134 km (83 mi). 1972 February 2 - 14:30 GMT - Launch Vehicle: M-100. M-100 TERLS-411 ISRO-8.58 Apogee: 91 km (56 mi). 1972 February 2 - 15:00 GMT - Launch Vehicle: M-100. Apogee: 91 km (56 mi). 1972 February 5 - 06:00 GMT - Launch Vehicle: Petrel. LV Model: Petrel 1 . Petrel P59T/C ISRO 18.07 Ionosphere mission Agency: SRC. Apogee: 139 km (86 mi). 1972 February 9 - 14:30 GMT - Launch Vehicle: M-100. M-100 TERLS-413 ISRO-8.59 Apogee: 85 km (52 mi). 1972 February 13 - 12:55 GMT - Launch Vehicle: Petrel. LV Model: Petrel 1 . Petrel P60T/C ISRO 18.08 Ionosphere mission Agency: SRC. Apogee: 137 km (85 mi). 1972 February 17 - 14:30 GMT - Launch Vehicle: M-100. M-100 TERLS-417 ISRO-8.60 Apogee: 90 km (55 mi). 1972 February 17 - 15:00 GMT - Launch Vehicle: M-100. Apogee: 90 km (55 mi). 1972 February 23 - 14:30 GMT - Launch Vehicle: M-100. M-100 TERLS-418 ISRO-8.61 Apogee: 88 km (54 mi). 1972 February 23 - 15:00 GMT - Launch Vehicle: M-100. Apogee: 87 km (54 mi). 1972 March 1 - 14:30 GMT - Launch Vehicle: M-100. M-100 TERLS-419 ISRO-8.62 Apogee: 85 km (52 mi). 1972 March 1 - 15:00 GMT - Launch Vehicle: M-100. Apogee: 90 km (55 mi). 1972 March 5 - 14:35 GMT - Launch Vehicle: Tomahawk Sandia. Sandhawk Tomahawk DLR T-DH-43 FAILURE: Failure. ISRO 21.01 Ionosphere mission Agency: ISRO/DLR. Apogee: 52 km (32 mi). 1972 March 8 - 15:00 GMT - Launch Vehicle: M-100. Apogee: 90 km (55 mi). 1972 March 8 - 16:30 GMT - Launch Vehicle: M-100. M-100 TERLS-421 ISRO-8.63 Apogee: 91 km (56 mi). 1972 March 11 - 14:38 GMT - Launch Vehicle: Tomahawk Sandia. Sandhawk Tomahawk DLT T-DH-44 FAILURE: Failure. ISRO 21.02 Ionosphere mission Agency: ISRO/DLR. Apogee: 52 km (32 mi). 1972 March 15 - 14:34 GMT - Launch Vehicle: M-100. M-100 TERLS-425 ISRO-8.64 Apogee: 89 km (55 mi). 1972 March 15 - 15:00 GMT - Launch Vehicle: M-100. Apogee: 91 km (56 mi). 1972 March 22 - 14:30 GMT - Launch Vehicle: M-100. Apogee: 91 km (56 mi). 1972 March 22 - 14:30 GMT - Launch Vehicle: M-100. M-100 TERLS-427 ISRO-8.65 Apogee: 92 km (57 mi). 1972 March 29 - 14:30 GMT - Launch Vehicle: M-100. M-100 TERLS-428 ISRO-8.66 Apogee: 90 km (55 mi). 1972 March 29 - 15:00 GMT - Launch Vehicle: M-100. Apogee: 90 km (55 mi). 1972 April 5 - 14:30 GMT - Launch Vehicle: M-100. M-100 TERLS-429 ISRO-8.67 Apogee: 91 km (56 mi). 1972 April 7 - 07:00 GMT - Launch Vehicle: Apache. Nike Apache NASA 14.412IP ISRO 10.43 Ionosphere mission Agency: NASA. Apogee: 147 km (91 mi). 1972 April 12 - 14:30 GMT - Launch Vehicle: M-100. M-100 TERLS-431 ISRO-8.68 Apogee: 85 km (52 mi). 1972 April 19 - 14:30 GMT - Launch Vehicle: M-100. M-100 TERLS-432 ISRO-8.69 Apogee: 87 km (54 mi). 1972 April 26 - 14:30 GMT - Launch Vehicle: M-100. M-100 TERLS-433 ISRO-8.70 Apogee: 85 km (52 mi). 1972 May 3 - 14:30 GMT - Launch Vehicle: M-100. M-100 TERLS-434 ISRO-8.71 Apogee: 92 km (57 mi). 1972 May 10 - 16:27 GMT - Launch Vehicle: M-100. M-100 TERLS-435 ISRO-8.72 Apogee: 91 km (56 mi). 1972 May 17 - 15:05 GMT - Launch Vehicle: M-100. M-100 TERLS-436 ISRO-8.73 Apogee: 88 km (54 mi). 1972 May 31 - 14:37 GMT - Launch Vehicle: M-100. M-100 TERLS-444 ISRO-8.74 Apogee: 90 km (55 mi). 1972 June 7 - 14:30 GMT - Launch Vehicle: M-100. M-100 TERLS-445 ISRO-8.75 Apogee: 90 km (55 mi). 1972 June 14 - 14:30 GMT - Launch Vehicle: M-100. M-100 TERLS-446 ISRO-8.76 Apogee: 89 km (55 mi). 1972 June 21 - 14:30 GMT - Launch Vehicle: M-100. M-100 TERLS-447 ISRO-8.77 Apogee: 90 km (55 mi). 1972 June 28 - 14:40 GMT - Launch Vehicle: M-100. M-100 TERLS-448 ISRO-8.78 Apogee: 88 km (54 mi). 1972 July 5 - 14:32 GMT - Launch Vehicle: M-100. M-100 TERLS-449 ISRO-8.79 Apogee: 87 km (54 mi). 1972 July 12 - 14:30 GMT - Launch Vehicle: M-100. M-100 TERLS-451 ISRO-8.80 Apogee: 87 km (54 mi). 1972 July 19 - 14:05 GMT - Launch Vehicle: M-100. M-100 TERLS-452 ISRO-8.81 Apogee: 89 km (55 mi). 1972 July 26 - 14:30 GMT - Launch Vehicle: M-100. M-100 TERLS-453 ISRO-8.82 Apogee: 89 km (55 mi). 1972 August 2 - 14:44 GMT - Launch Vehicle: M-100. M-100 TERLS-454 ISRO-8.83 Apogee: 88 km (54 mi). 1972 August 9 - 14:30 GMT - Launch Vehicle: M-100. M-100 TERLS-462 ISRO-8.84 Apogee: 87 km (54 mi). 1972 August 12 - 02:15 GMT - Launch Vehicle: Belier. Centaure ISRO 5.14 ISRO 5.14 Ionosphere mission Agency: ISRO. Apogee: 150 km (90 mi). 1972 August 13 - 06:59 GMT - Launch Vehicle: Apache. Nike Apache ISRO 10.44 ISRO 10.44 Ionosphere mission Agency: ISRO. Apogee: 148 km (91 mi). 1972 August 16 - 14:30 GMT - Launch Vehicle: M-100. M-100 TERLS-464 ISRO-8.85? Apogee: 88 km (54 mi). 1972 August 17 - 10:02 GMT - Launch Vehicle: Belier. Centaure ISRO 5.16 ISRO 5.16 Ionosphere mission Agency: ISRO. Apogee: 151 km (93 mi). 1972 August 24 - 14:30 GMT - Launch Vehicle: M-100. ISRO-8.86? Apogee: 87 km (54 mi). 1972 August 30 - 14:30 GMT - Launch Vehicle: M-100. M-100 TERLS-473 ISRO-8.87 Apogee: 90 km (55 mi). 1972 September 6 - 14:30 GMT - Launch Vehicle: M-100. M-100 TERLS-474 ISRO-8.88 Apogee: 87 km (54 mi). 1972 September 13 - 16:57 GMT - Launch Vehicle: M-100. M-100 TERLS-475 ISRO-8.89 Apogee: 86 km (53 mi). 1972 September 20 - 14:35 GMT - Launch Vehicle: M-100. M-100 TERLS-484 ISRO-8.90 Apogee: 86 km (53 mi). 1972 September 27 - 14:30 GMT - Launch Vehicle: M-100. M-100 TERLS-485 ISRO-8.91 Apogee: 87 km (54 mi). 1972 October 4 - 14:30 GMT - Launch Vehicle: M-100. M-100 TERLS-486 ISRO-8.92 Apogee: 89 km (55 mi). 1972 October 11 - 14:30 GMT - Launch Vehicle: M-100. M-100 TERLS-487 ISRO-8.93 Apogee: 90 km (55 mi). 1972 October 13 - 18:57 GMT - Launch Vehicle: Belier. Centaure 2A ISRO 5.17 ISRO 5.17 Fields mission Agency: ISRO. Apogee: 120 km (70 mi). 1972 October 18 - 15:06 GMT - Launch Vehicle: M-100. M-100 TERLS-490 ISRO-8.94 Apogee: 91 km (56 mi). 1972 October 25 - 14:30 GMT - Launch Vehicle: M-100. M-100 TERLS-497 ISRO-8.95 Apogee: 86 km (53 mi). 1972 November 1 - 14:44 GMT - Launch Vehicle: M-100. M-100 TERLS-498 ISRO-8.96 Apogee: 86 km (53 mi). 1972 November 9 - 14:30 GMT - Launch Vehicle: M-100. M-100 TERLS-499 ISRO-8.97 Apogee: 88 km (54 mi). 1972 November 15 - 14:30 GMT - Launch Vehicle: M-100. M-100 TERLS-500 ISRO-8.98 Apogee: 91 km (56 mi). 1972 November 22 - 14:30 GMT - Launch Vehicle: M-100. M-100 TERLS-501 ISRO-8.99 Apogee: 86 km (53 mi). 1972 November 29 - 14:30 GMT - Launch Vehicle: M-100. M-100 TERLS-502 ISRO-8.100 Apogee: 88 km (54 mi). 1972 December 6 - 14:33 GMT - Launch Vehicle: M-100. M-100 TERLS-503 ISRO-8.101 Apogee: 83 km (51 mi). 1972 December 13 - 14:30 GMT - Launch Vehicle: M-100. M-100 TERLS-504 ISRO-8.102 Apogee: 89 km (55 mi). 1972 December 20 - 14:30 GMT - Launch Vehicle: M-100. M-100 TERLS-509 ISRO-8.103 Apogee: 88 km (54 mi). 1972 December 27 - 14:30 GMT - Launch Vehicle: M-100. M-100 TERLS-510 ISRO-8.104 Apogee: 87 km (54 mi). 1973 January 3 - 14:30 GMT - Launch Vehicle: M-100. M-100 TERLS-511 ISRO-8.105 Apogee: 89 km (55 mi). 1973 January 3 - 15:50 GMT - Launch Vehicle: M-100. M-100 TERLS-512 ISRO-8.106 Apogee: 86 km (53 mi). 1973 January 10 - 14:30 GMT - Launch Vehicle: M-100. M-100 TERLS-517 ISRO-8.107 Apogee: 84 km (52 mi). 1973 January 11 - 16:10 GMT - Launch Vehicle: M-100. M-100 TERLS-518 ISRO-8.108 Apogee: 23 km (14 mi). 1973 January 17 - 14:30 GMT - Launch Vehicle: M-100. M-100 TERLS-519 ISRO-8.109 Apogee: 86 km (53 mi). 1973 January 21 - 09:40 GMT - Launch Vehicle: Belier. Centaure 2A ISRO 5.15 ISRO 5.15 Fields mission Agency: ISRO. Apogee: 165 km (102 mi). 1973 January 24 - 14:30 GMT - Launch Vehicle: M-100. M-100 TERLS-521 ISRO-8.110 Apogee: 90 km (55 mi). 1973 January 31 - 14:37 GMT - Launch Vehicle: M-100. M-100 TERLS-522 ISRO-8.111 Apogee: 85 km (52 mi). 1973 February 2 - 19:05 GMT - Launch Vehicle: Belier. Centaure 2A ISRO 5.18 ISRO 5.18 CO.07 Ionosphere mission Agency: ISRO. Apogee: 147 km (91 mi). 1973 February 8 - 14:35 GMT - Launch Vehicle: M-100. M-100 TERLS-524 ISRO-8.112 Apogee: 90 km (55 mi). 1973 February 22 - 14:30 GMT - Launch Vehicle: M-100. M-100 TERLS-529 ISRO-8.113 Apogee: 85 km (52 mi). 1973 February 27 - 15:00 GMT - Launch Vehicle: M-100. Apogee: 91 km (56 mi). 1973 February 28 - 14:30 GMT - Launch Vehicle: M-100. M-100 TERLS-530 ISRO-8.114 Apogee: 23 km (14 mi). 1973 March 1 - 14:50 GMT - Launch Vehicle: M-100. M-100 TERLS-531 ISRO-8.115 Apogee: 88 km (54 mi). 1973 March 3 - 06:05 GMT - Launch Vehicle: Belier. Centaure 2A ISRO 5.19 ISRO 5.19 Fields mission Agency: ISRO/CNES. Apogee: 125 km (77 mi). 1973 March 3 - 06:50 GMT - Launch Vehicle: Apache. Nike Apache ISRO 10.45 ISRO 10.45 Ionosphere mission Agency: ISRO. Apogee: 158 km (98 mi). 1973 March 7 - 14:30 GMT - Launch Vehicle: M-100. M-100 TERLS-534 ISRO-8.116 Apogee: 87 km (54 mi). 1973 March 14 - 14:50 GMT - Launch Vehicle: M-100. M-100 TERLS-545 ISRO-8.117 Apogee: 86 km (53 mi). 1973 March 21 - 14:30 GMT - Launch Vehicle: M-100. M-100 TERLS-548 ISRO-8.118 Apogee: 87 km (54 mi). 1973 March 28 - 14:30 GMT - Launch Vehicle: M-100. M-100 TERLS-549 ISRO-8.119 Apogee: 91 km (56 mi). 1973 April 4 - 14:30 GMT - Launch Vehicle: M-100. M-100 TERLS-550 ISRO-8.120 Apogee: 90 km (55 mi). 1973 April 11 - 14:00 GMT - Launch Vehicle: M-100. M-100 TERLS-551 ISRO-8.121 Apogee: 90 km (55 mi). 1973 April 11 - 17:50 GMT - Launch Vehicle: Belier. Centaure 2A ISRO 5.20 ISRO 5.20 Fields mission Agency: ISRO. Apogee: 151 km (93 mi). 1973 April 18 - 14:30 GMT - Launch Vehicle: M-100. M-100 TERLS-553 ISRO-8.122 Apogee: 84 km (52 mi). 1973 April 25 - 14:30 GMT - Launch Vehicle: M-100. M-100 TERLS-554 ISRO-8.123 Apogee: 89 km (55 mi). 1973 May 2 - 14:30 GMT - Launch Vehicle: M-100. M-100 TERLS-555 ISRO-8.124 Apogee: 84 km (52 mi). 1973 May 9 - 14:30 GMT - Launch Vehicle: M-100. M-100 TERLS-556 ISRO-8.125 Apogee: 88 km (54 mi). 1973 May 14 - 14:30 GMT - Launch Vehicle: M-100. M-100 TERLS-557 ISRO-8.126? Apogee: 86 km (53 mi). 1973 May 16 - 14:30 GMT - Launch Vehicle: M-100. M-100 TERLS-558 ISRO-8.127 Apogee: 84 km (52 mi). 1973 May 18 - 14:30 GMT - Launch Vehicle: M-100. M-100 TERLS-559 ISRO-8.128 Apogee: 88 km (54 mi). 1973 May 21 - 14:30 GMT - Launch Vehicle: M-100. M-100 TERLS-562 ISRO-8.129 Apogee: 87 km (54 mi). 1973 May 23 - 14:30 GMT - Launch Vehicle: M-100. M-100 TERLS-566 ISRO-8.130 Apogee: 89 km (55 mi). 1973 May 25 - 14:30 GMT - Launch Vehicle: M-100. M-100 TERLS-567 ISRO-8.131 Apogee: 90 km (55 mi). 1973 May 30 - 14:30 GMT - Launch Vehicle: M-100. M-100 TERLS-568 ISRO-8.132 Apogee: 86 km (53 mi). 1973 June 6 - 14:30 GMT - Launch Vehicle: M-100. M-100 TERLS-570 ISRO-8.133 Apogee: 88 km (54 mi). 1973 June 13 - 15:00 GMT - Launch Vehicle: M-100. Apogee: 87 km (54 mi). 1973 June 14 - 14:30 GMT - Launch Vehicle: M-100. M-100 TERLS-573 ISRO-8.134 Apogee: 83 km (51 mi). 1973 June 20 - 14:30 GMT - Launch Vehicle: M-100. M-100 TERLS-574 ISRO-8.135 Apogee: 88 km (54 mi). 1973 June 27 - 14:30 GMT - Launch Vehicle: M-100. M-100 TERLS-577 ISRO-8.136 Apogee: 88 km (54 mi). 1973 July 4 - 01:15 GMT - Launch Vehicle: Belier. Centaure 2A ISRO 5.21 ISRO 5.21 Fields mission Agency: ISRO. Apogee: 150 km (90 mi). 1973 July 4 - 14:30 GMT - Launch Vehicle: M-100. M-100 TERLS-579 ISRO-8.137 Apogee: 88 km (54 mi). 1973 July 11 - 14:30 GMT - Launch Vehicle: M-100. M-100 TERLS-580 ISRO-8.138 Apogee: 89 km (55 mi). 1973 July 18 - 14:30 GMT - Launch Vehicle: M-100. M-100 TERLS-583 ISRO-8.139 Apogee: 88 km (54 mi). 1973 July 25 - 14:30 GMT - Launch Vehicle: M-100. M-100 TERLS-584 ISRO-8.140 Apogee: 87 km (54 mi). 1973 August 1 - 14:30 GMT - Launch Vehicle: M-100. M-100 TERLS-587 ISRO-8.141 Apogee: 88 km (54 mi). 1973 August 8 - 14:30 GMT - Launch Vehicle: M-100. M-100 TERLS-588 ISRO-8.142 Apogee: 87 km (54 mi). 1973 August 16 - 14:30 GMT - Launch Vehicle: M-100. M-100 TERLS-589 ISRO-8.143 Apogee: 86 km (53 mi). 1973 August 22 - 14:30 GMT - Launch Vehicle: M-100. M-100 TERLS-590 ISRO-8.144 Apogee: 88 km (54 mi). 1973 August 29 - 14:30 GMT - Launch Vehicle: M-100. M-100 TERLS-593 ISRO-8.145 Apogee: 87 km (54 mi). 1973 September 5 - 14:30 GMT - Launch Vehicle: M-100. M-100 TERLS-594 ISRO-8.146 Apogee: 86 km (53 mi). 1973 September 12 - 14:30 GMT - Launch Vehicle: M-100. M-100 TERLS-595 ISRO-8.147 Apogee: 84 km (52 mi). 1973 September 19 - 14:30 GMT - Launch Vehicle: M-100. M-100 TERLS-596 ISRO-8.148 Apogee: 85 km (52 mi). 1973 September 27 - 14:30 GMT - Launch Vehicle: M-100. M-100 TERLS-597 ISRO-8.149 Apogee: 84 km (52 mi). 1973 October 3 - 14:30 GMT - Launch Vehicle: M-100. M-100 TERLS-598 ISRO-8.150 Apogee: 91 km (56 mi). 1973 October 10 - 14:30 GMT - Launch Vehicle: M-100. M-100 TERLS-599 ISRO-8.151 Apogee: 89 km (55 mi). 1973 October 17 - 14:30 GMT - Launch Vehicle: M-100. M-100 TERLS-600 ISRO-8.152 Apogee: 85 km (52 mi). 1973 October 24 - 14:30 GMT - Launch Vehicle: M-100. M-100 TERLS-601 ISRO-8.153 Apogee: 91 km (56 mi). 1973 October 31 - 14:30 GMT - Launch Vehicle: M-100. M-100 TERLS-602 ISRO-8.154 Apogee: 86 km (53 mi). 1973 November 7 - 14:30 GMT - Launch Vehicle: M-100. ISRO-8.155/TERLS-603 Apogee: 87 km (54 mi). 1973 November 14 - 14:30 GMT - Launch Vehicle: M-100. ISRO-8.156/TERLS-604 Apogee: 85 km (52 mi). 1973 November 17 - 14:30 GMT - Launch Vehicle: M-100. ISRO-8.157/TERLS-605 Apogee: 87 km (54 mi). 1973 November 21 - 15:15 GMT - Launch Vehicle: M-100. ISRO-8.158/TERLS-612 Apogee: 85 km (52 mi). 1973 November 24 - 14:30 GMT - Launch Vehicle: M-100. ISRO-8.159/TERLS-614 Apogee: 90 km (55 mi). 1973 November 28 - 14:38 GMT - Launch Vehicle: M-100. ISRO-8.160/TERLS-615 Apogee: 86 km (53 mi). 1973 December 1 - 14:30 GMT - Launch Vehicle: M-100. ISRO-8.161/TERLS-616 Apogee: 83 km (51 mi). 1973 December 5 - 14:30 GMT - Launch Vehicle: M-100. ISRO-8.162/TERLS-617 Apogee: 84 km (52 mi). 1973 December 12 - 14:30 GMT - Launch Vehicle: M-100. ISRO-8.163/TERLS-618 Apogee: 85 km (52 mi). 1973 December 15 - 14:30 GMT - Launch Vehicle: M-100. ISRO-8.164/TERLS-619 Apogee: 87 km (54 mi). 1973 December 19 - 14:30 GMT - Launch Vehicle: M-100. ISRO-8.165/TERLS-620 Apogee: 83 km (51 mi). 1973 December 26 - 14:30 GMT - Launch Vehicle: M-100. ISRO-8.166/TERLS-621 Apogee: 86 km (53 mi). 1974 January 2 - 14:30 GMT - Launch Vehicle: M-100. ISRO-8.167/TERLS-622 Apogee: 85 km (52 mi). 1974 January 9 - 14:30 GMT - Launch Vehicle: M-100. ISRO-8.168/TERLS-623 Apogee: 86 km (53 mi). 1974 January 16 - 15:00 GMT - Launch Vehicle: M-100. ISRO-8.169/TERLS-624 Apogee: 86 km (53 mi). 1974 January 23 - 14:30 GMT - Launch Vehicle: M-100. ISRO-8.170/TERLS-625 Apogee: 87 km (54 mi). 1974 January 30 - 14:30 GMT - Launch Vehicle: M-100. ISRO-8.171/TERLS-626 Apogee: 82 km (50 mi). 1974 February 6 - 14:30 GMT - Launch Vehicle: M-100. ISRO-8.172/TERLS-627 Apogee: 84 km (52 mi). 1974 February 13 - 14:30 GMT - Launch Vehicle: M-100. ISRO-8.173/TERLS-633 Apogee: 85 km (52 mi). 1974 February 20 - 14:30 GMT - Launch Vehicle: M-100. ISRO-8.174/TLERS-634 Apogee: 86 km (53 mi). 1974 February 27 - 16:00 GMT - Launch Vehicle: M-100. ISRO-8.175/TERLS-641 Apogee: 89 km (55 mi). 1974 March 6 - 15:00 GMT - Launch Vehicle: M-100. Apogee: 83 km (51 mi). 1974 March 13 - 15:00 GMT - Launch Vehicle: M-100. Apogee: 83 km (51 mi). 1974 March 20 - 15:00 GMT - Launch Vehicle: M-100. Apogee: 86 km (53 mi). 1974 March 27 - 15:00 GMT - Launch Vehicle: M-100. Apogee: 88 km (54 mi). 1974 April 3 - 16:00 GMT - Launch Vehicle: M-100. Apogee: 87 km (54 mi). 1974 April 10 - 15:00 GMT - Launch Vehicle: M-100. Apogee: 88 km (54 mi). 1974 April 17 - 15:00 GMT - Launch Vehicle: M-100. Apogee: 84 km (52 mi). 1974 April 24 - 16:00 GMT - Launch Vehicle: M-100. Apogee: 84 km (52 mi). 1974 May 1 - 15:00 GMT - Launch Vehicle: M-100. Apogee: 86 km (53 mi). 1974 May 8 - 15:00 GMT - Launch Vehicle: M-100. Apogee: 83 km (51 mi). 1974 May 16 - 15:00 GMT - Launch Vehicle: M-100. Apogee: 84 km (52 mi). 1974 May 22 - 15:00 GMT - Launch Vehicle: M-100. Apogee: 81 km (50 mi). 1974 May 29 - 15:00 GMT - Launch Vehicle: M-100. Apogee: 86 km (53 mi). 1974 June 1 - Launch Vehicle: M-100. Apogee: 80 km (49 mi). 1974 June 12 - 15:00 GMT - Launch Vehicle: M-100. Apogee: 84 km (52 mi). 1975 - Launch Vehicle: RH. First Flight test Agency: ISRO. Apogee: 130 km (80 mi). 1975 February 9 - 00:24 GMT - Launch Vehicle: Petrel. LV Model: Petrel 1 . Petrel P154T/C ISRO-18.09 Atmospheric mission Agency: SRC. Apogee: 165 km (102 mi). 1975 February 9 - 00:24 GMT - Launch Vehicle: Petrel. LV Model: Petrel 1 . Petrel P155T/C Electrojet ISRO-18.12 Atmospheric mission Agency: SRC. Apogee: 170 km (100 mi). 1975 February 9 - 00:29 GMT - Launch Vehicle: Petrel. LV Model: Petrel 1 . Petrel P158T/C ISRO-18.10 Ionosphere mission Agency: SRC. Apogee: 130 km (80 mi). 1975 February 9 - 05:30 GMT - Launch Vehicle: Petrel. LV Model: Petrel 1 . Petrel P137T/C ISRO-18.11 Ionosphere mission Agency: SRC. Apogee: 102 km (63 mi). 1975 February 9 - 05:50 GMT - Launch Vehicle: Belier. Centaure ISRO 5.23 CE-1 ISRO 5.23 Ionosphere mission Agency: ISRO. Apogee: 150 km (90 mi). 1975 February 9 - 07:08 GMT - Launch Vehicle: Petrel. LV Model: Petrel 1 . Petrel P159T/C ISRO-18.13 Ionosphere mission Agency: SRC. Apogee: 130 km (80 mi). 1975 February 19 - 05:35 GMT - Launch Vehicle: Belier. Centaure ISRO 5.25 CE-4 ISRO 5.25 CO.04 Ionosphere mission Agency: ISRO. Apogee: 160 km (90 mi). 1975 February 19 - 08:37 GMT - Launch Vehicle: Petrel. LV Model: Petrel 1 . Petrel P156T/C ISRO-18.15 Atmospheric mission Agency: SRC. Apogee: 170 km (100 mi). 1975 February 19 - 08:42 GMT - Launch Vehicle: Petrel. LV Model: Petrel 1 . Petrel P138T/C ISRO-18.14 Ionosphere mission Agency: SRC. Apogee: 135 km (83 mi). 1975 February 19 - 09:04 GMT - Launch Vehicle: Belier. Centaure ISRO 5.24 CE-2 ISRO 5.24 Ionosphere mission Agency: ISRO. Apogee: 164 km (101 mi). 1975 February 19 - 13:32 GMT - Launch Vehicle: Petrel. LV Model: Petrel 1 . Petrel P157T/C ISRO-18.16 Atmospheric mission Agency: SRC. Apogee: 165 km (102 mi). 1975 March 15 - 16:34 GMT - Launch Vehicle: Petrel. LV Model: Petrel 1 . Petrel P70T/C ISRO-18.17 Ionosphere mission Agency: SRC. Apogee: 147 km (91 mi). 1975 March 16 - 00:00 GMT - Launch Vehicle: Petrel. LV Model: Petrel 1 . Petrel P184T/C ISRO-18.18 Ionosphere mission Agency: SRC. Apogee: 120 km (70 mi). 1975 March 19 - 09:21 GMT - Launch Vehicle: Petrel. LV Model: Petrel 1 . Petrel P185T/C ISRO-18.19 Ionosphere mission Agency: SRC. Apogee: 107 km (66 mi). 1975 March 24 - 00:06 GMT - Launch Vehicle: Petrel. LV Model: Petrel 1 . Petrel P160T/C ISRO-18.20 Fields mission Agency: SRC. Apogee: 90 km (55 mi). 1975 April 21 - 08:11 GMT - Launch Vehicle: Belier. Centaure ISRO 5.26 ISRO 5.26 CO.22 Ionosphere mission Agency: ISRO. Apogee: 157 km (97 mi). 1975 April 21 - 17:30 GMT - Launch Vehicle: Belier. Centaure ISRO 5.27 ISRO 5.27 CO.21 Ionosphere mission Agency: ISRO. Apogee: 156 km (96 mi). 1975 May 19 - 15:00 GMT - Launch Vehicle: M-100. Apogee: 89 km (55 mi). 1975 May 21 - 15:00 GMT - Launch Vehicle: M-100. Apogee: 86 km (53 mi). 1975 May 23 - 15:00 GMT - Launch Vehicle: M-100. Apogee: 86 km (53 mi). 1975 May 26 - 15:00 GMT - Launch Vehicle: M-100. Apogee: 84 km (52 mi). 1975 May 28 - 14:40 GMT - Launch Vehicle: M-100. Apogee: 84 km (52 mi). 1975 May 30 - 16:00 GMT - Launch Vehicle: M-100. Apogee: 86 km (53 mi). 1975 June 4 - 15:00 GMT - Launch Vehicle: M-100. Apogee: 88 km (54 mi). 1975 June 11 - 15:00 GMT - Launch Vehicle: M-100. Apogee: 88 km (54 mi). 1975 June 18 - 15:00 GMT - Launch Vehicle: M-100. Apogee: 88 km (54 mi). 1975 June 25 - 15:00 GMT - Launch Vehicle: M-100. Apogee: 88 km (54 mi). 1975 July 2 - 15:00 GMT - Launch Vehicle: M-100. Apogee: 87 km (54 mi). 1975 July 8 - 06:00 GMT - Launch Vehicle: RH. Gerdien probe Aeronomy mission Agency: ISRO. Apogee: 40 km (24 mi). 1975 July 9 - 15:00 GMT - Launch Vehicle: M-100. Apogee: 87 km (54 mi). 1975 July 16 - 15:00 GMT - Launch Vehicle: M-100. Apogee: 87 km (54 mi). 1975 July 23 - 15:00 GMT - Launch Vehicle: M-100. Apogee: 87 km (54 mi). 1975 July 30 - 15:00 GMT - Launch Vehicle: M-100. Apogee: 88 km (54 mi). 1975 August 6 - 15:00 GMT - Launch Vehicle: M-100. Apogee: 87 km (54 mi). 1975 August 13 - 15:00 GMT - Launch Vehicle: M-100. Apogee: 89 km (55 mi). 1975 August 19 - 15:00 GMT - Launch Vehicle: M-100. Apogee: 87 km (54 mi). 1975 August 27 - 15:00 GMT - Launch Vehicle: M-100. Apogee: 84 km (52 mi). 1975 September 3 - 15:00 GMT - Launch Vehicle: M-100. Apogee: 85 km (52 mi). 1975 September 10 - 15:00 GMT - Launch Vehicle: M-100. Apogee: 84 km (52 mi). 1975 September 17 - 15:00 GMT - Launch Vehicle: M-100. Apogee: 87 km (54 mi). 1975 September 24 - 15:00 GMT - Launch Vehicle: M-100. Apogee: 88 km (54 mi). 1975 October 1 - 15:00 GMT - Launch Vehicle: M-100. Apogee: 83 km (51 mi). 1975 October 8 - 15:00 GMT - Launch Vehicle: M-100. Apogee: 86 km (53 mi). 1975 October 15 - 15:00 GMT - Launch Vehicle: M-100. Apogee: 85 km (52 mi). 1975 October 22 - 15:00 GMT - Launch Vehicle: M-100. Apogee: 85 km (52 mi). 1975 October 29 - 15:00 GMT - Launch Vehicle: M-100. Apogee: 84 km (52 mi). 1975 November 5 - 15:00 GMT - Launch Vehicle: M-100. Apogee: 83 km (51 mi). 1975 November 11 - 15:00 GMT - Launch Vehicle: M-100. Apogee: 85 km (52 mi). 1975 November 19 - 15:00 GMT - Launch Vehicle: M-100. Apogee: 91 km (56 mi). 1975 December 3 - 15:00 GMT - Launch Vehicle: M-100. Apogee: 83 km (51 mi). 1975 December 6 - 06:30 GMT - Launch Vehicle: M-100. Apogee: 85 km (52 mi). 1975 December 10 - 15:00 GMT - Launch Vehicle: M-100. Apogee: 90 km (55 mi). 1975 December 17 - 15:00 GMT - Launch Vehicle: M-100. Apogee: 87 km (54 mi). 1975 December 18 - 15:00 GMT - Launch Vehicle: M-100. Apogee: 87 km (54 mi). 1975 December 24 - 15:00 GMT - Launch Vehicle: M-100. Apogee: 84 km (52 mi). 1975 December 31 - 15:00 GMT - Launch Vehicle: M-100. Apogee: 81 km (50 mi). 1976 January 7 - 14:30 GMT - Launch Vehicle: M-100. ISRO-8.230 Apogee: 83 km (51 mi). 1976 January 14 - 14:30 GMT - Launch Vehicle: M-100. ISRO-8.231 Aeronomy mission Apogee: 88 km (54 mi). 1976 January 21 - 14:30 GMT - Launch Vehicle: M-100. ISRO-8.232 Aeronomy mission Apogee: 83 km (51 mi). 1976 January 28 - 14:30 GMT - Launch Vehicle: M-100. ISRO-8.233 Aeronomy mission Apogee: 85 km (52 mi). 1976 February 4 - 14:30 GMT - Launch Vehicle: M-100. ISRO-8.234 Aeronomy mission Apogee: 84 km (52 mi). 1976 February 11 - 14:30 GMT - Launch Vehicle: M-100. ISRO-8.235 Apogee: 83 km (51 mi). 1976 February 12 - 14:30 GMT - Launch Vehicle: M-100. ISRO-8.236 Apogee: 86 km (53 mi). 1976 February 18 - 14:30 GMT - Launch Vehicle: M-100. ISRO-8.237 Apogee: 91 km (56 mi). 1976 February 25 - 16:00 GMT - Launch Vehicle: M-100. ISRO-8.238 Apogee: 87 km (54 mi). 1976 February 29 - 13:04 GMT - Launch Vehicle: Belier. Centaure 2B ISRO 5.29 ISRO 5.29 Aeronomy / ionosphere mission Agency: ISRO. Apogee: 56 km (34 mi). 1976 March 3 - 14:30 GMT - Launch Vehicle: M-100. ISRO-8.239 Apogee: 84 km (52 mi). 1976 March 10 - 14:30 GMT - Launch Vehicle: M-100. ISRO-8.240 Apogee: 85 km (52 mi). 1976 March 17 - 14:30 GMT - Launch Vehicle: M-100. ISRO-8.241 Apogee: 78 km (48 mi). 1976 March 24 - 00:40 GMT - Launch Vehicle: Belier. Centaure 2B ISRO 5.30 ISRO 5.30 Ionosphere / fields mission Agency: ISRO. Apogee: 142 km (88 mi). 1976 March 24 - 16:23 GMT - Launch Vehicle: M-100. ISRO-8.242 Apogee: 86 km (53 mi). 1976 March 26 - 01:25 GMT - Launch Vehicle: Belier. Centaure 2B ISRO 5.31 ISRO 5.31 Ionosphere / fields mission Agency: ISRO. Apogee: 139 km (86 mi). 1976 March 31 - 14:35 GMT - Launch Vehicle: M-100. ISRO-8.243 Apogee: 90 km (55 mi). 1976 April 7 - 14:30 GMT - Launch Vehicle: M-100. ISRO-8.244 Apogee: 88 km (54 mi). 1976 April 14 - 14:30 GMT - Launch Vehicle: M-100. ISRO-8.245 Apogee: 83 km (51 mi). 1976 April 18 - 23:55 GMT - Launch Vehicle: Belier. Centaure 2B ISRO 5.32 ISRO 5.32 Aeronomy / ionosphere mission Agency: ISRO. Apogee: 152 km (94 mi). 1976 April 21 - 14:30 GMT - Launch Vehicle: M-100. ISRO-8.246 Apogee: 88 km (54 mi). 1976 April 28 - 14:30 GMT - Launch Vehicle: M-100. ISRO-8.247 Apogee: 87 km (54 mi). 1976 May 5 - 14:30 GMT - Launch Vehicle: M-100. ISRO-8.248 Apogee: 85 km (52 mi). 1976 May 12 - 14:30 GMT - Launch Vehicle: M-100. ISRO-8.249 Apogee: 88 km (54 mi). 1976 May 19 - 14:30 GMT - Launch Vehicle: M-100. ISRO-8.250 Apogee: 75 km (46 mi). 1976 May 21 - 14:35 GMT - Launch Vehicle: M-100. ISRO-8.251 Apogee: 86 km (53 mi). 1976 May 24 - 14:30 GMT - Launch Vehicle: M-100. ISRO-8.252 Apogee: 84 km (52 mi). 1976 May 26 - 14:30 GMT - Launch Vehicle: M-100. ISRO-8.253 Apogee: 86 km (53 mi). 1976 May 28 - 14:33 GMT - Launch Vehicle: M-100. ISRO-8.254 Apogee: 83 km (51 mi). 1976 May 31 - 14:30 GMT - Launch Vehicle: M-100. ISRO-8.255 Apogee: 83 km (51 mi). 1976 June 2 - 14:38 GMT - Launch Vehicle: M-100. ISRO-8.256 Apogee: 85 km (52 mi). 1976 June 9 - 15:12 GMT - Launch Vehicle: M-100. ISRO-8.257 Apogee: 85 km (52 mi). 1976 June 16 - 14:30 GMT - Launch Vehicle: M-100. ISRO-8.258 Apogee: 56 km (34 mi). 1976 June 23 - 14:35 GMT - Launch Vehicle: M-100. ISRO-8.259 Apogee: 79 km (49 mi). 1976 June 30 - 14:34 GMT - Launch Vehicle: M-100. ISRO-8.260 Apogee: 85 km (52 mi). 1976 July 7 - 15:00 GMT - Launch Vehicle: M-100. ISRO-8.261 Apogee: 86 km (53 mi). 1976 July 14 - 14:50 GMT - Launch Vehicle: M-100. ISRO-8.262 Apogee: 85 km (52 mi). 1976 July 21 - 14:45 GMT - Launch Vehicle: M-100. ISRO-8.263 Apogee: 85 km (52 mi). 1976 July 27 - 04:45 GMT - Launch Vehicle: Belier. Centaure 2B ISRO 5.33 ISRO 5.33 test Agency: ISRO. Apogee: 97 km (60 mi). 1976 July 28 - 14:30 GMT - Launch Vehicle: M-100. ISRO-8.264 Apogee: 83 km (51 mi). 1976 August 4 - 14:33 GMT - Launch Vehicle: M-100. ISRO-8.265 Apogee: 84 km (52 mi). 1976 August 11 - 14:30 GMT - Launch Vehicle: M-100. ISRO-8.266 Apogee: 85 km (52 mi). 1976 August 18 - 14:30 GMT - Launch Vehicle: M-100. ISRO-8.267 Aeronomy mission Apogee: 85 km (52 mi). 1976 August 18 - 20:30 GMT - Launch Vehicle: M-100. ISRO-8.268 Aeronomy mission Apogee: 83 km (51 mi). 1976 August 19 - 02:30 GMT - Launch Vehicle: M-100. ISRO-8.269 Aeronomy mission Apogee: 84 km (52 mi). 1976 August 19 - 08:47 GMT - Launch Vehicle: M-100. ISRO-8.270 Aeronomy mission Apogee: 83 km (51 mi). 1976 August 19 - 14:30 GMT - Launch Vehicle: M-100. ISRO-8.271 Aeronomy mission Apogee: 68 km (42 mi). 1976 August 19 - 15:48 GMT - Launch Vehicle: M-100. ISRO-8.272 Aeronomy mission Apogee: 85 km (52 mi). 1976 August 19 - 20:30 GMT - Launch Vehicle: M-100. ISRO-8.273 Aeronomy mission Apogee: 84 km (52 mi). 1976 August 20 - 02:30 GMT - Launch Vehicle: M-100. ISRO-8.274 Aeronomy mission Apogee: 86 km (53 mi). 1976 August 20 - 08:25 GMT - Launch Vehicle: M-100. ISRO-8.275 Aeronomy mission Apogee: 86 km (53 mi). 1976 August 25 - 14:30 GMT - Launch Vehicle: M-100. ISRO-8.276 Apogee: 80 km (49 mi). 1976 September 1 - 14:30 GMT - Launch Vehicle: M-100. ISRO-8.277 Apogee: 81 km (50 mi). 1976 September 9 - 14:30 GMT - Launch Vehicle: M-100. ISRO-8.278 Apogee: 84 km (52 mi). 1976 September 15 - 14:30 GMT - Launch Vehicle: M-100. ISRO-8.279 Apogee: 84 km (52 mi). 1976 September 22 - 14:54 GMT - Launch Vehicle: M-100. ISRO-8.280 Apogee: 86 km (53 mi). 1976 September 23 - 14:30 GMT - Launch Vehicle: M-100. ISRO-8.281 Apogee: 87 km (54 mi). 1976 September 25 - 07:15 GMT - Launch Vehicle: M-100. ISRO-8.282 Apogee: 90 km (55 mi). 1976 September 29 - 14:30 GMT - Launch Vehicle: M-100. ISRO-8.283 Apogee: 86 km (53 mi). 1976 October 6 - 14:30 GMT - Launch Vehicle: M-100. ISRO-8.284 Apogee: 66 km (41 mi). 1976 October 8 - 17:44 GMT - Launch Vehicle: Belier. Centaure 2B ISRO 5.34 ISRO 5.34 Plasma mission Agency: ISRO. Apogee: 120 km (70 mi). 1976 October 13 - 14:30 GMT - Launch Vehicle: M-100. ISRO-8.285 Apogee: 80 km (49 mi). 1976 October 14 - 17:17 GMT - Launch Vehicle: Belier. Centaure 2B ISRO 5.35 FAILURE: Failure. ISRO 5.35 Plasma mission Agency: ISRO. Apogee: 0 km ( mi). 1976 October 20 - 14:30 GMT - Launch Vehicle: M-100. ISRO-8.286 Apogee: 82 km (50 mi). 1976 October 27 - 14:30 GMT - Launch Vehicle: M-100. ISRO-8.287 Apogee: 82 km (50 mi). 1976 October 27 - 16:29 GMT - Launch Vehicle: Belier. Centaure 2B ISRO 5.36 C.34 ISRO 5.36 C-300 X-ray astronomy mission Agency: ISRO. Apogee: 148 km (91 mi). 1976 November 3 - 14:30 GMT - Launch Vehicle: M-100. ISRO-8.288 Apogee: 83 km (51 mi). 1976 November 10 - 15:00 GMT - Launch Vehicle: M-100. ISRO-8.289 Apogee: 83 km (51 mi). 1976 November 17 - 14:30 GMT - Launch Vehicle: M-100. ISRO-8.290 Apogee: 85 km (52 mi). 1976 November 18 - 04:25 GMT - Launch Vehicle: Belier. Centaure 2B ISRO 5.37 ISRO 5.37 Ionosphere mission Agency: ISRO. Apogee: 128 km (79 mi). 1976 November 24 - 14:30 GMT - Launch Vehicle: M-100. ISRO-8.291 Apogee: 82 km (50 mi). 1976 December 1 - 14:30 GMT - Launch Vehicle: M-100. ISRO-8.292 Apogee: 81 km (50 mi). 1976 December 8 - 14:30 GMT - Launch Vehicle: M-100. ISRO-8.293 Apogee: 86 km (53 mi). 1976 December 16 - 14:30 GMT - Launch Vehicle: M-100. ISRO-8.294 Apogee: 85 km (52 mi). 1976 December 22 - 14:30 GMT - Launch Vehicle: M-100. ISRO-8.295 Apogee: 81 km (50 mi). 1976 December 29 - 14:30 GMT - Launch Vehicle: M-100. ISRO-8.296 Apogee: 83 km (51 mi). 1977 - Launch Vehicle: RH. Parachute test Agency: ISRO. Apogee: 40 km (24 mi). 1977 January 5 - 15:00 GMT - Launch Vehicle: M-100. Apogee: 81 km (50 mi). 1977 January 12 - 15:00 GMT - Launch Vehicle: M-100. Apogee: 85 km (52 mi). 1977 January 19 - 15:00 GMT - Launch Vehicle: M-100. Apogee: 81 km (50 mi). 1977 January 27 - 15:00 GMT - Launch Vehicle: M-100. Apogee: 85 km (52 mi). 1977 February 2 - 15:00 GMT - Launch Vehicle: M-100. Apogee: 86 km (53 mi). 1977 February 9 - 15:00 GMT - Launch Vehicle: M-100. Apogee: 36 km (22 mi). 1977 February 10 - 15:00 GMT - Launch Vehicle: M-100. Apogee: 85 km (52 mi). 1977 February 17 - 15:00 GMT - Launch Vehicle: M-100. Apogee: 84 km (52 mi). 1977 February 23 - 15:00 GMT - Launch Vehicle: M-100. Apogee: 83 km (51 mi). 1977 March 2 - 15:00 GMT - Launch Vehicle: M-100. Apogee: 81 km (50 mi). 1977 March 9 - 15:00 GMT - Launch Vehicle: M-100. Apogee: 84 km (52 mi). 1977 March 16 - 15:00 GMT - Launch Vehicle: M-100. Apogee: 78 km (48 mi). 1977 March 23 - 15:00 GMT - Launch Vehicle: M-100. Apogee: 75 km (46 mi). 1977 March 30 - 15:00 GMT - Launch Vehicle: M-100. Apogee: 81 km (50 mi). 1977 April 6 - 15:00 GMT - Launch Vehicle: M-100. Apogee: 87 km (54 mi). 1977 April 13 - 15:00 GMT - Launch Vehicle: M-100. Apogee: 85 km (52 mi). 1977 April 20 - 15:00 GMT - Launch Vehicle: M-100. Apogee: 80 km (49 mi). 1977 April 27 - 15:00 GMT - Launch Vehicle: M-100. Apogee: 85 km (52 mi). 1977 May 4 - 15:00 GMT - Launch Vehicle: M-100. Apogee: 84 km (52 mi). 1977 May 11 - 15:00 GMT - Launch Vehicle: M-100. Apogee: 84 km (52 mi). 1977 May 14 - 14:00 GMT - Launch Vehicle: M-100. Apogee: 82 km (50 mi). 1977 May 16 - 15:00 GMT - Launch Vehicle: M-100. Apogee: 84 km (52 mi). 1977 May 18 - 15:00 GMT - Launch Vehicle: M-100. Apogee: 84 km (52 mi). 1977 May 20 - 15:00 GMT - Launch Vehicle: M-100. Apogee: 84 km (52 mi). 1977 May 23 - 15:00 GMT - Launch Vehicle: M-100. Apogee: 81 km (50 mi). 1977 May 25 - 15:00 GMT - Launch Vehicle: M-100. Apogee: 64 km (39 mi). 1977 May 27 - 15:00 GMT - Launch Vehicle: M-100. Apogee: 76 km (47 mi). 1977 May 30 - 15:00 GMT - Launch Vehicle: M-100. Apogee: 84 km (52 mi). 1977 June 1 - 15:00 GMT - Launch Vehicle: M-100. Apogee: 90 km (55 mi). 1977 June 1 - 15:00 GMT - Launch Vehicle: M-100. Apogee: 87 km (54 mi). 1977 June 4 - 05:58 GMT - Launch Vehicle: Belier. Centaure 2B ISRO ISRO CO.40 Ionosphere mission Agency: ISRO. Apogee: 150 km (90 mi). 1977 June 8 - 15:00 GMT - Launch Vehicle: M-100. Apogee: 83 km (51 mi). 1977 June 15 - 15:00 GMT - Launch Vehicle: M-100. Apogee: 83 km (51 mi). 1977 June 22 - 15:00 GMT - Launch Vehicle: M-100. Apogee: 80 km (49 mi). 1977 June 29 - 15:00 GMT - Launch Vehicle: M-100. Apogee: 76 km (47 mi). 1977 July 6 - 15:00 GMT - Launch Vehicle: M-100. Apogee: 79 km (49 mi). 1977 July 13 - 15:00 GMT - Launch Vehicle: M-100. Apogee: 83 km (51 mi). 1977 July 20 - 14:00 GMT - Launch Vehicle: M-100. Apogee: 84 km (52 mi). 1977 July 27 - 14:00 GMT - Launch Vehicle: M-100. Apogee: 85 km (52 mi). 1977 August 3 - 14:00 GMT - Launch Vehicle: M-100. Apogee: 90 km (55 mi). 1977 August 10 - 07:00 GMT - Launch Vehicle: M-100. Apogee: 72 km (44 mi). 1977 August 17 - 14:00 GMT - Launch Vehicle: M-100. Apogee: 69 km (42 mi). 1977 August 24 - 14:00 GMT - Launch Vehicle: M-100. Apogee: 88 km (54 mi). 1977 August 31 - 15:00 GMT - Launch Vehicle: M-100. Apogee: 84 km (52 mi). 1977 September 7 - 14:00 GMT - Launch Vehicle: M-100. Apogee: 84 km (52 mi). 1977 September 14 - 14:00 GMT - Launch Vehicle: M-100. Apogee: 67 km (41 mi). 1977 September 22 - 14:00 GMT - Launch Vehicle: M-100. Apogee: 78 km (48 mi). 1977 September 28 - 14:00 GMT - Launch Vehicle: M-100. Apogee: 85 km (52 mi). 1977 September 29 - 14:00 GMT - Launch Vehicle: M-100. Apogee: 87 km (54 mi). 1977 October 5 - 05:00 GMT - Launch Vehicle: M-100. Apogee: 90 km (55 mi). 1977 October 5 - 15:00 GMT - Launch Vehicle: M-100. Apogee: 85 km (52 mi). 1977 October 5 - 17:00 GMT - Launch Vehicle: M-100. Apogee: 81 km (50 mi). 1977 October 11 - 14:00 GMT - Launch Vehicle: M-100. Apogee: 82 km (50 mi). 1977 October 19 - 14:00 GMT - Launch Vehicle: M-100. Apogee: 82 km (50 mi). 1977 October 26 - 16:00 GMT - Launch Vehicle: M-100. Apogee: 79 km (49 mi). 1977 November 2 - 16:00 GMT - Launch Vehicle: M-100. Apogee: 85 km (52 mi). 1977 November 10 - 15:00 GMT - Launch Vehicle: M-100. Apogee: 86 km (53 mi). 1977 November 16 - 15:00 GMT - Launch Vehicle: M-100. Apogee: 86 km (53 mi). 1977 November 22 - 15:00 GMT - Launch Vehicle: M-100. Apogee: 82 km (50 mi). 1977 November 28 - 15:00 GMT - Launch Vehicle: M-100. Apogee: 85 km (52 mi). 1978 January 4 - 14:00 GMT - Launch Vehicle: M-100. Apogee: 86 km (53 mi). 1978 January 11 - 14:00 GMT - Launch Vehicle: M-100. Apogee: 86 km (53 mi). 1978 January 18 - 14:00 GMT - Launch Vehicle: M-100. Apogee: 86 km (53 mi). 1978 January 25 - 14:00 GMT - Launch Vehicle: M-100. Apogee: 82 km (50 mi). 1978 February 1 - 14:00 GMT - Launch Vehicle: M-100. Apogee: 82 km (50 mi). 1978 February 8 - 14:00 GMT - Launch Vehicle: M-100. Apogee: 83 km (51 mi). 1978 February 15 - 14:00 GMT - Launch Vehicle: M-100. Apogee: 81 km (50 mi). 1978 February 21 - 09:22 GMT - Launch Vehicle: Belier. Centaure 2B ISRO ISRO CO.47 Ionosphere mission Agency: ISRO. Apogee: 150 km (90 mi). 1978 February 22 - 14:00 GMT - Launch Vehicle: M-100. Apogee: 85 km (52 mi). 1978 March 1 - 14:00 GMT - Launch Vehicle: M-100. Apogee: 83 km (51 mi). 1978 March 8 - 14:00 GMT - Launch Vehicle: M-100. Apogee: 84 km (52 mi). 1978 March 15 - 14:00 GMT - Launch Vehicle: M-100. Apogee: 83 km (51 mi). 1978 March 22 - 14:00 GMT - Launch Vehicle: M-100. Apogee: 85 km (52 mi). 1978 March 29 - 14:00 GMT - Launch Vehicle: M-100. Apogee: 85 km (52 mi). 1978 April 18 - Launch Vehicle: RH. AST 1 Technology mission Agency: ISRO. Apogee: 130 km (80 mi). 1978 April 20 - 17:00 GMT - Launch Vehicle: M-100. Apogee: 80 km (49 mi). 1978 May 10 - 14:00 GMT - Launch Vehicle: M-100. Apogee: 81 km (50 mi). 1978 May 15 - 14:00 GMT - Launch Vehicle: M-100. Apogee: 75 km (46 mi). 1978 May 17 - 14:00 GMT - Launch Vehicle: M-100. Apogee: 82 km (50 mi). 1978 May 19 - 14:00 GMT - Launch Vehicle: M-100. Apogee: 81 km (50 mi). 1978 May 23 - 14:00 GMT - Launch Vehicle: M-100. Apogee: 81 km (50 mi). 1978 May 29 - 14:00 GMT - Launch Vehicle: M-100. Apogee: 81 km (50 mi). 1978 May 31 - 14:00 GMT - Launch Vehicle: M-100. Apogee: 81 km (50 mi). 1978 June 2 - 14:00 GMT - Launch Vehicle: M-100. Apogee: 84 km (52 mi). 1978 June 7 - 14:00 GMT - Launch Vehicle: M-100. Apogee: 82 km (50 mi). 1978 June 14 - 14:00 GMT - Launch Vehicle: M-100. Apogee: 78 km (48 mi). 1978 June 14 - 14:33 GMT - Launch Vehicle: M-100. Apogee: 78 km (48 mi). 1978 June 22 - 14:00 GMT - Launch Vehicle: M-100. Apogee: 84 km (52 mi). 1978 June 22 - 14:12 GMT - Launch Vehicle: M-100. Apogee: 84 km (52 mi). 1978 June 28 - 14:00 GMT - Launch Vehicle: M-100. Apogee: 83 km (51 mi). 1978 July 5 - 14:00 GMT - Launch Vehicle: M-100. Apogee: 76 km (47 mi). 1978 July 12 - 14:00 GMT - Launch Vehicle: M-100. Apogee: 85 km (52 mi). 1978 July 12 - 14:07 GMT - Launch Vehicle: M-100. Apogee: 85 km (52 mi). 1978 July 13 - 14:00 GMT - Launch Vehicle: M-100. Apogee: 84 km (52 mi). 1978 July 19 - 14:34 GMT - Launch Vehicle: M-100. Apogee: 82 km (50 mi). 1978 July 19 - 15:00 GMT - Launch Vehicle: M-100. Apogee: 82 km (50 mi). 1978 July 26 - 14:00 GMT - Launch Vehicle: M-100. Apogee: 82 km (50 mi). 1978 August 2 - 15:00 GMT - Launch Vehicle: M-100. Apogee: 84 km (52 mi). 1978 August 9 - 14:00 GMT - Launch Vehicle: M-100. Apogee: 83 km (51 mi). 1978 August 9 - 15:00 GMT - Launch Vehicle: M-100. Apogee: 83 km (51 mi). 1978 August 16 - 14:00 GMT - Launch Vehicle: M-100. Apogee: 74 km (45 mi). 1978 August 23 - 14:00 GMT - Launch Vehicle: M-100. Apogee: 84 km (52 mi). 1978 August 23 - 14:12 GMT - Launch Vehicle: M-100. Apogee: 85 km (52 mi). 1978 August 30 - 14:00 GMT - Launch Vehicle: M-100. Apogee: 84 km (52 mi). 1978 September 4 - 04:30 GMT - Launch Vehicle: M-100. Apogee: 89 km (55 mi). 1978 September 5 - 14:00 GMT - Launch Vehicle: M-100. Apogee: 87 km (54 mi). 1978 September 12 - 14:00 GMT - Launch Vehicle: M-100. Apogee: 85 km (52 mi). 1978 September 21 - 14:00 GMT - Launch Vehicle: M-100. Apogee: 84 km (52 mi). 1978 September 27 - 14:00 GMT - Launch Vehicle: M-100. Apogee: 87 km (54 mi). 1978 October 4 - 14:00 GMT - Launch Vehicle: M-100. Apogee: 84 km (52 mi). 1978 October 11 - 14:00 GMT - Launch Vehicle: M-100. Apogee: 85 km (52 mi). 1978 October 18 - 14:00 GMT - Launch Vehicle: M-100. Apogee: 83 km (51 mi). 1978 October 25 - 14:00 GMT - Launch Vehicle: M-100. Apogee: 83 km (51 mi). 1978 November 1 - 15:00 GMT - Launch Vehicle: M-100. Apogee: 81 km (50 mi). 1978 November 8 - 15:00 GMT - Launch Vehicle: M-100. Apogee: 86 km (53 mi). 1978 November 15 - 14:00 GMT - Launch Vehicle: M-100. Apogee: 86 km (53 mi). 1978 November 22 - 15:00 GMT - Launch Vehicle: M-100. Apogee: 84 km (52 mi). 1978 November 30 - 14:00 GMT - Launch Vehicle: M-100. Apogee: 83 km (51 mi). 1978 December 6 - 14:00 GMT - Launch Vehicle: M-100. Apogee: 81 km (50 mi). 1978 December 13 - 14:00 GMT - Launch Vehicle: M-100. Apogee: 81 km (50 mi). 1978 December 20 - 14:00 GMT - Launch Vehicle: M-100. Apogee: 85 km (52 mi). 1978 December 20 - 20:45 GMT - Launch Vehicle: Belier. Centaure 2B ISRO ISRO C.51 Ionosphere mission Agency: ISRO. Apogee: 160 km (90 mi). 1978 December 21 - 00:45 GMT - Launch Vehicle: Belier. Centaure 2B ISRO ISRO CO.52 Ionosphere mission Agency: ISRO. Apogee: 135 km (83 mi). 1978 December 27 - 14:00 GMT - Launch Vehicle: M-100. Apogee: 87 km (54 mi). 1979 January 3 - 14:00 GMT - Launch Vehicle: M-100. Apogee: 86 km (53 mi). 1979 January 10 - 14:00 GMT - Launch Vehicle: M-100. Apogee: 84 km (52 mi). 1979 January 12 - 14:00 GMT - Launch Vehicle: M-100. Apogee: 86 km (53 mi). 1979 January 17 - 16:00 GMT - Launch Vehicle: M-100. Apogee: 74 km (45 mi). 1979 January 19 - 14:00 GMT - Launch Vehicle: M-100. Apogee: 86 km (53 mi). 1979 January 24 - 14:00 GMT - Launch Vehicle: M-100. Apogee: 85 km (52 mi). 1979 January 27 - 14:00 GMT - Launch Vehicle: M-100. Apogee: 83 km (51 mi). 1979 January 31 - 14:00 GMT - Launch Vehicle: M-100. Apogee: 86 km (53 mi). 1979 February 2 - 14:00 GMT - Launch Vehicle: M-100. Apogee: 86 km (53 mi). 1979 February 7 - 15:00 GMT - Launch Vehicle: M-100. Apogee: 83 km (51 mi). 1979 February 9 - 14:00 GMT - Launch Vehicle: M-100. Apogee: 83 km (51 mi). 1979 February 14 - 14:00 GMT - Launch Vehicle: M-100. Apogee: 84 km (52 mi). 1979 February 16 - 14:00 GMT - Launch Vehicle: M-100. Apogee: 84 km (52 mi). 1979 February 21 - 16:00 GMT - Launch Vehicle: M-100. Apogee: 86 km (53 mi). 1979 February 28 - 14:00 GMT - Launch Vehicle: M-100. Apogee: 80 km (49 mi). 1979 March 8 - 14:00 GMT - Launch Vehicle: M-100. Apogee: 83 km (51 mi). 1979 March 14 - 12:00 GMT - Launch Vehicle: M-100. Apogee: 85 km (52 mi). 1979 March 16 - 12:00 GMT - Launch Vehicle: M-100. Apogee: 83 km (51 mi). 1979 March 18 - 12:00 GMT - Launch Vehicle: M-100. Apogee: 84 km (52 mi). 1979 March 19 - 11:40 GMT - Launch Vehicle: M-100. Apogee: 85 km (52 mi). 1979 March 20 - 11:40 GMT - Launch Vehicle: M-100. Apogee: 86 km (53 mi). 1979 March 21 - 11:40 GMT - Launch Vehicle: M-100. Apogee: 85 km (52 mi). 1979 March 22 - 11:45 GMT - Launch Vehicle: M-100. Apogee: 86 km (53 mi). 1979 March 24 - 12:00 GMT - Launch Vehicle: M-100. Apogee: 86 km (53 mi). 1979 March 24 - 14:00 GMT - Launch Vehicle: M-100. Apogee: 85 km (52 mi). 1979 March 26 - 11:40 GMT - Launch Vehicle: M-100. Apogee: 84 km (52 mi). 1979 March 28 - 11:40 GMT - Launch Vehicle: M-100. Apogee: 85 km (52 mi). 1979 March 30 - 11:40 GMT - Launch Vehicle: M-100. Apogee: 85 km (52 mi). 1979 April 1 - 12:00 GMT - Launch Vehicle: M-100. Apogee: 85 km (52 mi). 1979 April 3 - 12:00 GMT - Launch Vehicle: M-100. Apogee: 86 km (53 mi). 1979 April 5 - 12:00 GMT - Launch Vehicle: M-100. Apogee: 85 km (52 mi). 1979 April 7 - 12:00 GMT - Launch Vehicle: M-100. Apogee: 85 km (52 mi). 1979 April 7 - 14:00 GMT - Launch Vehicle: M-100. Apogee: 84 km (52 mi). 1979 April 9 - 06:00 GMT - Launch Vehicle: M-100. Apogee: 95 km (59 mi). 1979 April 9 - 12:00 GMT - Launch Vehicle: M-100. Apogee: 85 km (52 mi). 1979 April 11 - 11:00 GMT - Launch Vehicle: M-100. Apogee: 85 km (52 mi). 1979 April 14 - 12:01 GMT - Launch Vehicle: M-100. Apogee: 83 km (51 mi). 1979 April 18 - 14:00 GMT - Launch Vehicle: M-100. Apogee: 83 km (51 mi). 1979 April 19 - 14:00 GMT - Launch Vehicle: M-100. Apogee: 82 km (50 mi). 1979 April 25 - 14:00 GMT - Launch Vehicle: M-100. Apogee: 85 km (52 mi). 1979 May 2 - 11:30 GMT - Launch Vehicle: M-100. Apogee: 82 km (50 mi). 1979 May 9 - 14:00 GMT - Launch Vehicle: M-100. Apogee: 84 km (52 mi). 1979 May 16 - 09:40 GMT - Launch Vehicle: M-100. Apogee: 94 km (58 mi). 1979 May 16 - 14:00 GMT - Launch Vehicle: M-100. Apogee: 88 km (54 mi). 1979 May 18 - 14:40 GMT - Launch Vehicle: M-100. Apogee: 81 km (50 mi). 1979 May 23 - 14:00 GMT - Launch Vehicle: M-100. Apogee: 83 km (51 mi). 1979 May 25 - 14:00 GMT - Launch Vehicle: M-100. Apogee: 83 km (51 mi). 1979 May 30 - 14:40 GMT - Launch Vehicle: M-100. Apogee: 86 km (53 mi). 1979 June 1 - 14:00 GMT - Launch Vehicle: M-100. Apogee: 85 km (52 mi). 1979 June 8 - 11:40 GMT - Launch Vehicle: M-100. Apogee: 82 km (50 mi). 1979 June 13 - 14:00 GMT - Launch Vehicle: M-100. Apogee: 82 km (50 mi). 1979 June 20 - 14:00 GMT - Launch Vehicle: M-100. Apogee: 86 km (53 mi). 1979 June 27 - 14:00 GMT - Launch Vehicle: M-100. Apogee: 84 km (52 mi). 1979 July 11 - 12:00 GMT - Launch Vehicle: M-100. Apogee: 85 km (52 mi). 1979 July 18 - 14:00 GMT - Launch Vehicle: M-100. Apogee: 83 km (51 mi). 1979 July 20 - 14:00 GMT - Launch Vehicle: M-100. Apogee: 85 km (52 mi). 1979 July 25 - 14:00 GMT - Launch Vehicle: M-100. Apogee: 86 km (53 mi). 1979 July 27 - 15:00 GMT - Launch Vehicle: M-100. Apogee: 84 km (52 mi). 1979 August 1 - 14:00 GMT - Launch Vehicle: M-100. Apogee: 86 km (53 mi). 1979 August 3 - 15:00 GMT - Launch Vehicle: M-100. Apogee: 83 km (51 mi). 1979 August 8 - 15:00 GMT - Launch Vehicle: M-100. Apogee: 85 km (52 mi). 1979 August 10 - 14:00 GMT - Launch Vehicle: M-100. Apogee: 85 km (52 mi). 1979 August 14 - 15:00 GMT - Launch Vehicle: M-100. Apogee: 84 km (52 mi). 1979 August 17 - 12:00 GMT - Launch Vehicle: M-100. Apogee: 88 km (54 mi). 1979 August 22 - 14:00 GMT - Launch Vehicle: M-100. Apogee: 84 km (52 mi). 1979 August 24 - 14:00 GMT - Launch Vehicle: M-100. Apogee: 86 km (53 mi). 1979 August 25 - 06:21 GMT - Launch Vehicle: RH. ISRO-CNES I Ionosphere mission Agency: ISRO. Apogee: 150 km (90 mi). 1979 August 29 - 15:00 GMT - Launch Vehicle: M-100. Apogee: 87 km (54 mi). 1979 August 31 - 05:51 GMT - Launch Vehicle: RH. ISRO-CNES II Ionosphere mission Agency: ISRO. Apogee: 150 km (90 mi). 1979 September 6 - 12:00 GMT - Launch Vehicle: M-100. Apogee: 82 km (50 mi). 1979 September 12 - 14:00 GMT - Launch Vehicle: M-100. Apogee: 87 km (54 mi). 1979 September 19 - 14:00 GMT - Launch Vehicle: M-100. Apogee: 85 km (52 mi). 1979 November 15 - Launch Vehicle: Belier. AST 2 Technology test Agency: ISRO. Apogee: 148 km (91 mi). 1979 November 28 - 14:00 GMT - Launch Vehicle: M-100. Apogee: 91 km (56 mi). 1979 December 6 - 14:00 GMT - Launch Vehicle: M-100. Apogee: 89 km (55 mi). 1979 December 12 - 11:40 GMT - Launch Vehicle: M-100. Apogee: 89 km (55 mi). 1979 December 19 - 14:00 GMT - Launch Vehicle: M-100. Apogee: 89 km (55 mi). 1979 December 26 - 14:00 GMT - Launch Vehicle: M-100. Apogee: 89 km (55 mi). 1980 January 2 - 11:00 GMT - Launch Vehicle: M-100. Apogee: 85 km (52 mi). 1980 January 4 - 14:00 GMT - Launch Vehicle: M-100. Apogee: 84 km (52 mi). 1980 January 7 - 14:00 GMT - Launch Vehicle: M-100. Apogee: 86 km (53 mi). 1980 January 9 - 14:00 GMT - Launch Vehicle: M-100. Apogee: 85 km (52 mi). 1980 January 11 - 14:00 GMT - Launch Vehicle: M-100. Apogee: 85 km (52 mi). 1980 January 14 - 15:00 GMT - Launch Vehicle: M-100. Apogee: 82 km (50 mi). 1980 January 16 - 14:00 GMT - Launch Vehicle: M-100. Apogee: 81 km (50 mi). 1980 January 18 - 14:00 GMT - Launch Vehicle: M-100. Apogee: 83 km (51 mi). 1980 January 21 - 14:00 GMT - Launch Vehicle: M-100. Apogee: 84 km (52 mi). 1980 January 23 - 14:00 GMT - Launch Vehicle: M-100. Apogee: 86 km (53 mi). 1980 January 25 - 15:00 GMT - Launch Vehicle: M-100. Apogee: 84 km (52 mi). 1980 January 28 - 14:00 GMT - Launch Vehicle: M-100. Apogee: 86 km (53 mi). 1980 January 30 - 14:00 GMT - Launch Vehicle: M-100. Apogee: 84 km (52 mi). 1980 February 6 - 14:00 GMT - Launch Vehicle: M-100. Apogee: 85 km (52 mi). 1980 February 7 - 14:00 GMT - Launch Vehicle: M-100. Apogee: 85 km (52 mi). 1980 February 13 - 14:00 GMT - Launch Vehicle: M-100. Apogee: 85 km (52 mi). 1980 February 16 - 07:23 GMT - Launch Vehicle: M-100. M-100 ISRO 8.506 Meteorological Meteorological / eclipse mission Apogee: 84 km (52 mi). 1980 February 16 - 09:24 GMT - Launch Vehicle: Belier. Centaure 2B ISRO 5.60 Eclipse D1 Eclipse ionosphere mission Agency: ISRO. Apogee: 140 km (80 mi). 1980 February 16 - 09:52 GMT - Launch Vehicle: Belier. Centaure 2B ISRO 5.61 Eclipse D2 Eclipse ionosphere mission Agency: ISRO. Apogee: 140 km (80 mi). 1980 February 16 - 11:05 GMT - Launch Vehicle: M-100. M-100 ISRO 8.507 Meteorological Meteorological / eclipse mission Apogee: 86 km (53 mi). 1980 February 16 - 13:25 GMT - Launch Vehicle: Belier. Centaure 2B ISRO 5.63 Eclipse Ba / Li Eclipse aeronomy mission Agency: ISRO. Apogee: 140 km (80 mi). 1980 February 17 - Launch Vehicle: Belier. Centaure 2B ISRO 5.65/C.59 NO Photometer Aeronomy mission Agency: ISRO. Apogee: 150 km (90 mi). 1980 February 17 - 09:52 GMT - Launch Vehicle: Belier. Centaure 2B ISRO 5.64 Eclipse D3 Eclipse ionosphere mission Agency: ISRO. Apogee: 140 km (80 mi). 1980 February 18 - 01:50 GMT - Launch Vehicle: Belier. O3 Photometer Aeronomy mission Agency: ISRO. Apogee: 100 km (60 mi). 1980 February 20 - 16:00 GMT - Launch Vehicle: M-100. Apogee: 88 km (54 mi). 1980 February 27 - 14:00 GMT - Launch Vehicle: M-100. Apogee: 85 km (52 mi). 1980 March 5 - 14:00 GMT - Launch Vehicle: M-100. Apogee: 84 km (52 mi). 1980 March 6 - 14:00 GMT - Launch Vehicle: M-100. Apogee: 88 km (54 mi). 1980 March 12 - 14:00 GMT - Launch Vehicle: M-100. Apogee: 85 km (52 mi). 1980 March 19 - 14:00 GMT - Launch Vehicle: M-100. Apogee: 87 km (54 mi). 1980 March 26 - 14:00 GMT - Launch Vehicle: M-100. Apogee: 83 km (51 mi). 1980 April 2 - 12:00 GMT - Launch Vehicle: M-100. Apogee: 85 km (52 mi). 1980 April 9 - 02:20 GMT - Launch Vehicle: M-100. Apogee: 83 km (51 mi). 1980 April 9 - 06:00 GMT - Launch Vehicle: M-100. Apogee: 84 km (52 mi). 1980 April 9 - 10:00 GMT - Launch Vehicle: M-100. Apogee: 85 km (52 mi). 1980 April 9 - 14:00 GMT - Launch Vehicle: M-100. Apogee: 84 km (52 mi). 1980 April 9 - 18:00 GMT - Launch Vehicle: M-100. Apogee: 82 km (50 mi). 1980 April 9 - 21:00 GMT - Launch Vehicle: M-100. Apogee: 84 km (52 mi). 1980 April 10 - 02:00 GMT - Launch Vehicle: M-100. Apogee: 85 km (52 mi). 1980 April 10 - 06:00 GMT - Launch Vehicle: M-100. Apogee: 85 km (52 mi). 1980 April 10 - 10:04 GMT - Launch Vehicle: M-100. Apogee: 84 km (52 mi). 1980 April 10 - 14:00 GMT - Launch Vehicle: M-100. Apogee: 82 km (50 mi). 1980 April 10 - 18:00 GMT - Launch Vehicle: M-100. Apogee: 82 km (50 mi). 1980 April 10 - 21:00 GMT - Launch Vehicle: M-100. Apogee: 83 km (51 mi). 1980 April 11 - 02:00 GMT - Launch Vehicle: M-100. Apogee: 84 km (52 mi). 1980 April 11 - 06:00 GMT - Launch Vehicle: M-100. Apogee: 83 km (51 mi). 1980 April 23 - 14:00 GMT - Launch Vehicle: M-100. Apogee: 84 km (52 mi). 1980 April 29 - 14:00 GMT - Launch Vehicle: M-100. Apogee: 85 km (52 mi). 1980 May 7 - 11:40 GMT - Launch Vehicle: M-100. Apogee: 82 km (50 mi). 1980 May 14 - 14:00 GMT - Launch Vehicle: M-100. Apogee: 83 km (51 mi). 1980 May 21 - 14:00 GMT - Launch Vehicle: M-100. Apogee: 83 km (51 mi). 1980 May 28 - 14:00 GMT - Launch Vehicle: M-100. Apogee: 82 km (50 mi). 1980 June 4 - 12:00 GMT - Launch Vehicle: M-100. Apogee: 83 km (51 mi). 1980 June 12 - 14:00 GMT - Launch Vehicle: M-100. Apogee: 82 km (50 mi). 1980 June 19 - 14:00 GMT - Launch Vehicle: M-100. Apogee: 83 km (51 mi). 1980 June 26 - 14:00 GMT - Launch Vehicle: M-100. Apogee: 82 km (50 mi). 1980 July 2 - 14:00 GMT - Launch Vehicle: M-100. Apogee: 83 km (51 mi). 1980 July 9 - 14:00 GMT - Launch Vehicle: M-100. Apogee: 86 km (53 mi). 1980 July 16 - 14:00 GMT - Launch Vehicle: M-100. Apogee: 83 km (51 mi). 1980 July 23 - 14:00 GMT - Launch Vehicle: M-100. Apogee: 84 km (52 mi). 1980 July 30 - 14:00 GMT - Launch Vehicle: M-100. Apogee: 83 km (51 mi). 1980 August 13 - 14:00 GMT - Launch Vehicle: M-100. Apogee: 84 km (52 mi). 1980 August 16 - 11:50 GMT - Launch Vehicle: M-100. Apogee: 86 km (53 mi). 1980 August 20 - 14:00 GMT - Launch Vehicle: M-100. Apogee: 82 km (50 mi). 1980 August 27 - 14:00 GMT - Launch Vehicle: M-100. Apogee: 82 km (50 mi). 1980 September 3 - 12:15 GMT - Launch Vehicle: M-100. Apogee: 83 km (51 mi). 1980 September 10 - 14:00 GMT - Launch Vehicle: M-100. Apogee: 84 km (52 mi). 1980 September 17 - 14:00 GMT - Launch Vehicle: M-100. Apogee: 86 km (53 mi). 1980 September 24 - 09:30 GMT - Launch Vehicle: M-100. M-100 Ozone M-08-554 ISRO-8.554 Aeronomy mission Agency: ISRO. Apogee: 81 km (50 mi). 1980 September 24 - 14:00 GMT - Launch Vehicle: M-100. Apogee: 83 km (51 mi). 1980 September 24 - 21:30 GMT - Launch Vehicle: M-100. M-100 Ozone M-08-556 ISRO-8.556 Aeronomy mission Agency: ISRO. Apogee: 81 km (50 mi). 1980 October 1 - 14:00 GMT - Launch Vehicle: M-100. Apogee: 78 km (48 mi). 1980 October 8 - 14:00 GMT - Launch Vehicle: M-100. Apogee: 84 km (52 mi). 1980 October 15 - 14:00 GMT - Launch Vehicle: M-100. Apogee: 87 km (54 mi). 1980 October 22 - 14:00 GMT - Launch Vehicle: M-100. Apogee: 78 km (48 mi). 1980 October 29 - 14:00 GMT - Launch Vehicle: M-100. Apogee: 82 km (50 mi). 1980 November 5 - 14:00 GMT - Launch Vehicle: M-100. Apogee: 84 km (52 mi). 1980 November 12 - 14:50 GMT - Launch Vehicle: M-100. Apogee: 80 km (49 mi). 1980 November 20 - 14:00 GMT - Launch Vehicle: M-100. Apogee: 86 km (53 mi). 1980 November 26 - 14:00 GMT - Launch Vehicle: M-100. Apogee: 86 km (53 mi). 1980 December 3 - 14:10 GMT - Launch Vehicle: M-100. Apogee: 86 km (53 mi). 1980 December 10 - 13:00 GMT - Launch Vehicle: M-100. Apogee: 86 km (53 mi). 1980 December 17 - 14:00 GMT - Launch Vehicle: M-100. Apogee: 82 km (50 mi). 1980 December 24 - 14:00 GMT - Launch Vehicle: M-100. Apogee: 85 km (52 mi). 1980 December 31 - 14:00 GMT - Launch Vehicle: M-100. Apogee: 83 km (51 mi). 1981 January 7 - 14:00 GMT - Launch Vehicle: M-100. Apogee: 87 km (54 mi). 1981 January 14 - 14:00 GMT - Launch Vehicle: M-100. Apogee: 81 km (50 mi). 1981 January 21 - 14:00 GMT - Launch Vehicle: M-100. Apogee: 85 km (52 mi). 1981 January 28 - 14:00 GMT - Launch Vehicle: M-100. Apogee: 83 km (51 mi). 1981 February 4 - 05:00 GMT - Launch Vehicle: Belier. Centaure ISRO C.76 Langmuir / E Field Ionosphere mission Agency: ISRO. Apogee: 150 km (90 mi). 1981 February 11 - 14:00 GMT - Launch Vehicle: M-100. Apogee: 87 km (54 mi). 1981 February 12 - 05:27 GMT - Launch Vehicle: Belier. Centaure 2B ISRO C.77 Langmuir / E Field Ionosphere mission Agency: ISRO. Apogee: 158 km (98 mi). 1981 February 18 - 14:00 GMT - Launch Vehicle: M-100. Apogee: 81 km (50 mi). 1981 February 25 - 14:00 GMT - Launch Vehicle: M-100. Apogee: 81 km (50 mi). 1981 March 4 - 14:00 GMT - Launch Vehicle: M-100. Apogee: 82 km (50 mi). 1981 March 11 - 14:00 GMT - Launch Vehicle: M-100. Apogee: 83 km (51 mi). 1981 March 18 - 14:00 GMT - Launch Vehicle: M-100. Apogee: 72 km (44 mi). 1981 March 25 - 14:00 GMT - Launch Vehicle: M-100. Apogee: 85 km (52 mi). 1981 April 1 - 14:10 GMT - Launch Vehicle: M-100. Apogee: 85 km (52 mi). 1981 April 8 - 14:00 GMT - Launch Vehicle: M-100. Apogee: 70 km (43 mi). 1981 April 15 - 14:00 GMT - Launch Vehicle: M-100. Apogee: 84 km (52 mi). 1981 April 22 - 14:00 GMT - Launch Vehicle: M-100. Apogee: 87 km (54 mi). 1981 April 29 - 14:00 GMT - Launch Vehicle: M-100. Apogee: 85 km (52 mi). 1981 May 3 - 14:00 GMT - Launch Vehicle: M-100. Apogee: 85 km (52 mi). 1981 May 6 - 14:00 GMT - Launch Vehicle: M-100. Apogee: 84 km (52 mi). 1981 May 13 - 14:00 GMT - Launch Vehicle: M-100. Apogee: 85 km (52 mi). 1981 May 15 - 14:00 GMT - Launch Vehicle: M-100. Apogee: 85 km (52 mi). 1981 May 20 - 16:30 GMT - Launch Vehicle: M-100. Apogee: 85 km (52 mi). 1981 May 22 - 16:30 GMT - Launch Vehicle: M-100. Apogee: 84 km (52 mi). 1981 May 27 - 14:00 GMT - Launch Vehicle: M-100. Apogee: 63 km (39 mi). 1981 May 29 - 14:00 GMT - Launch Vehicle: M-100. Apogee: 87 km (54 mi). 1981 June 5 - 14:00 GMT - Launch Vehicle: M-100. Apogee: 80 km (49 mi). 1981 June 10 - 14:00 GMT - Launch Vehicle: M-100. Apogee: 80 km (49 mi). 1981 June 17 - 14:00 GMT - Launch Vehicle: M-100. Apogee: 79 km (49 mi). 1981 June 24 - 14:00 GMT - Launch Vehicle: M-100. Apogee: 84 km (52 mi). 1981 July 1 - 14:00 GMT - Launch Vehicle: M-100. Apogee: 84 km (52 mi). 1981 July 8 - 14:00 GMT - Launch Vehicle: M-100. Apogee: 84 km (52 mi). 1981 July 15 - 14:00 GMT - Launch Vehicle: M-100. Apogee: 82 km (50 mi). 1981 July 22 - 14:00 GMT - Launch Vehicle: M-100. Apogee: 86 km (53 mi). 1981 July 29 - 14:00 GMT - Launch Vehicle: M-100. Apogee: 83 km (51 mi). 1981 August 5 - 14:00 GMT - Launch Vehicle: M-100. Apogee: 85 km (52 mi). 1981 August 12 - 14:00 GMT - Launch Vehicle: M-100. Apogee: 84 km (52 mi). 1981 August 19 - 14:00 GMT - Launch Vehicle: M-100. Apogee: 82 km (50 mi). 1981 August 26 - 14:00 GMT - Launch Vehicle: M-100. Apogee: 86 km (53 mi). 1981 September 2 - 14:00 GMT - Launch Vehicle: M-100. Apogee: 85 km (52 mi). 1981 September 9 - 14:00 GMT - Launch Vehicle: M-100. Apogee: 73 km (45 mi). 1981 September 17 - 14:00 GMT - Launch Vehicle: M-100. Apogee: 84 km (52 mi). 1981 September 22 - 14:20 GMT - Launch Vehicle: M-100. Apogee: 83 km (51 mi). 1981 September 30 - 14:00 GMT - Launch Vehicle: M-100. Apogee: 84 km (52 mi). 1981 October 7 - 14:00 GMT - Launch Vehicle: M-100. Apogee: 84 km (52 mi). 1981 October 14 - 14:00 GMT - Launch Vehicle: M-100. Apogee: 85 km (52 mi). 1981 October 21 - 14:00 GMT - Launch Vehicle: M-100. Apogee: 84 km (52 mi). 1981 October 28 - 14:00 GMT - Launch Vehicle: M-100. Apogee: 83 km (51 mi). 1981 November 2 - 14:00 GMT - Launch Vehicle: M-100. Apogee: 84 km (52 mi). 1981 November 4 - 14:00 GMT - Launch Vehicle: M-100. Apogee: 85 km (52 mi). 1981 November 11 - 09:20 GMT - Launch Vehicle: M-100. Apogee: 82 km (50 mi). 1981 November 11 - 14:00 GMT - Launch Vehicle: M-100. Apogee: 84 km (52 mi). 1981 November 11 - 21:35 GMT - Launch Vehicle: M-100. M-100 Ozone M-08-621 ISRO-8.621 Aeronomy mission Agency: ISRO. Apogee: 82 km (50 mi). 1981 November 12 - 09:30 GMT - Launch Vehicle: M-100. M-100 Ozone M-08-622 ISRO-8.622 Aeronomy mission Agency: ISRO. Apogee: 84 km (52 mi). 1981 November 16 - 15:40 GMT - Launch Vehicle: M-100. Apogee: 83 km (51 mi). 1981 November 18 - 14:00 GMT - Launch Vehicle: M-100. Apogee: 85 km (52 mi). 1981 November 23 - 14:00 GMT - Launch Vehicle: M-100. Apogee: 83 km (51 mi). 1981 November 25 - 15:40 GMT - Launch Vehicle: M-100. Apogee: 85 km (52 mi). 1981 November 30 - 14:00 GMT - Launch Vehicle: M-100. Apogee: 84 km (52 mi). 1981 December 1 - Launch Vehicle: M-100. Apogee: 80 km (49 mi). 1981 December 1 - Launch Vehicle: M-100. Apogee: 80 km (49 mi). 1981 December 1 - Launch Vehicle: M-100. Apogee: 80 km (49 mi). 1981 December 1 - Launch Vehicle: M-100. Apogee: 80 km (49 mi). 1981 December 9 - 14:00 GMT - Launch Vehicle: M-100. Apogee: 88 km (54 mi). 1982 January 6 - 14:40 GMT - Launch Vehicle: M-100. Apogee: 81 km (50 mi). 1982 January 14 - 14:00 GMT - Launch Vehicle: M-100. Apogee: 86 km (53 mi). 1982 January 20 - 14:00 GMT - Launch Vehicle: M-100. Apogee: 84 km (52 mi). 1982 January 27 - 14:00 GMT - Launch Vehicle: M-100. Apogee: 85 km (52 mi). 1982 January 30 - 05:59 GMT - Launch Vehicle: Belier. Centaure ISRO C.73 Langmuir / E Field Ionosphere mission Agency: ISRO. Apogee: 150 km (90 mi). 1982 February 1 - Launch Vehicle: RH. Thermistor test / Meteorological mission Agency: ISRO. Apogee: 70 km (43 mi). 1982 February 3 - 14:00 GMT - Launch Vehicle: M-100. Apogee: 83 km (51 mi). 1982 February 10 - 14:00 GMT - Launch Vehicle: M-100. Apogee: 84 km (52 mi). 1982 February 17 - 14:00 GMT - Launch Vehicle: M-100. Apogee: 83 km (51 mi). 1982 February 24 - 15:00 GMT - Launch Vehicle: M-100. Apogee: 83 km (51 mi). 1982 March 1 - Launch Vehicle: RH. Thermistor test / Meteorological mission Agency: ISRO. Apogee: 70 km (43 mi). 1982 March 1 - Launch Vehicle: RH. Thermistor test / Meteorological mission Agency: ISRO. Apogee: 70 km (43 mi). 1982 March 3 - 15:00 GMT - Launch Vehicle: M-100. Apogee: 86 km (53 mi). 1982 March 10 - 14:00 GMT - Launch Vehicle: M-100. Apogee: 87 km (54 mi). 1982 March 17 - 14:20 GMT - Launch Vehicle: M-100. Apogee: 85 km (52 mi). 1982 March 24 - 14:00 GMT - Launch Vehicle: M-100. Apogee: 82 km (50 mi). 1982 March 31 - 14:00 GMT - Launch Vehicle: M-100. Apogee: 85 km (52 mi). 1982 April 1 - Launch Vehicle: RH. Thermistor test / Meteorological mission Agency: ISRO. Apogee: 70 km (43 mi). 1982 April 7 - 14:00 GMT - Launch Vehicle: M-100. Apogee: 83 km (51 mi). 1982 April 14 - 14:00 GMT - Launch Vehicle: M-100. Apogee: 82 km (50 mi). 1982 April 21 - 14:00 GMT - Launch Vehicle: M-100. Apogee: 82 km (50 mi). 1982 April 28 - 14:00 GMT - Launch Vehicle: M-100. Apogee: 84 km (52 mi). 1982 May 5 - 14:00 GMT - Launch Vehicle: M-100. Apogee: 82 km (50 mi). 1982 May 12 - 14:00 GMT - Launch Vehicle: M-100. Apogee: 85 km (52 mi). 1982 May 20 - 14:00 GMT - Launch Vehicle: M-100. Apogee: 81 km (50 mi). 1982 May 26 - 14:00 GMT - Launch Vehicle: M-100. Apogee: 81 km (50 mi). 1982 June 2 - 14:00 GMT - Launch Vehicle: M-100. Apogee: 84 km (52 mi). 1982 June 9 - 14:00 GMT - Launch Vehicle: M-100. Apogee: 85 km (52 mi). 1982 June 16 - 14:00 GMT - Launch Vehicle: M-100. Apogee: 83 km (51 mi). 1982 June 23 - 14:00 GMT - Launch Vehicle: M-100. Apogee: 84 km (52 mi). 1982 July 1 - 14:00 GMT - Launch Vehicle: M-100. Apogee: 84 km (52 mi). 1982 July 7 - 14:00 GMT - Launch Vehicle: M-100. Apogee: 82 km (50 mi). 1982 July 14 - 14:00 GMT - Launch Vehicle: M-100. Apogee: 84 km (52 mi). 1982 July 21 - 14:00 GMT - Launch Vehicle: M-100. Apogee: 87 km (54 mi). 1982 July 28 - 14:00 GMT - Launch Vehicle: M-100. Apogee: 87 km (54 mi). 1982 August 4 - 14:00 GMT - Launch Vehicle: M-100. Apogee: 82 km (50 mi). 1982 August 11 - 14:00 GMT - Launch Vehicle: M-100. Apogee: 84 km (52 mi). 1982 August 18 - 14:00 GMT - Launch Vehicle: M-100. Apogee: 82 km (50 mi). 1982 August 25 - 14:00 GMT - Launch Vehicle: M-100. Apogee: 90 km (55 mi). 1982 September 2 - 14:00 GMT - Launch Vehicle: M-100. Apogee: 85 km (52 mi). 1982 September 8 - 14:00 GMT - Launch Vehicle: M-100. Apogee: 84 km (52 mi). 1982 September 15 - 14:00 GMT - Launch Vehicle: M-100. Apogee: 85 km (52 mi). 1982 September 22 - 14:00 GMT - Launch Vehicle: M-100. Apogee: 89 km (55 mi). 1982 September 30 - 14:00 GMT - Launch Vehicle: M-100. Apogee: 81 km (50 mi). 1982 October 6 - 14:00 GMT - Launch Vehicle: M-100. Apogee: 81 km (50 mi). 1982 October 13 - 14:00 GMT - Launch Vehicle: M-100. Apogee: 82 km (50 mi). 1982 October 20 - 14:00 GMT - Launch Vehicle: M-100. Apogee: 85 km (52 mi). 1982 October 27 - 14:00 GMT - Launch Vehicle: M-100. Apogee: 84 km (52 mi). 1982 November 3 - 14:00 GMT - Launch Vehicle: M-100. Apogee: 82 km (50 mi). 1982 November 10 - 14:00 GMT - Launch Vehicle: M-100. Apogee: 70 km (43 mi). 1982 November 17 - 14:00 GMT - Launch Vehicle: M-100. Apogee: 85 km (52 mi). 1982 November 24 - 14:00 GMT - Launch Vehicle: M-100. Apogee: 85 km (52 mi). 1982 November 25 - 14:00 GMT - Launch Vehicle: M-100. Apogee: 85 km (52 mi). 1982 November 29 - 05:21 GMT - Launch Vehicle: M-100. Gerdien probe Aeronomy mission Agency: ISRO. Apogee: 85 km (52 mi). 1982 December 1 - 14:00 GMT - Launch Vehicle: M-100. Apogee: 85 km (52 mi). 1982 December 2 - 14:00 GMT - Launch Vehicle: M-100. Apogee: 85 km (52 mi). 1982 December 8 - 14:41 GMT - Launch Vehicle: M-100. Apogee: 79 km (49 mi). 1982 December 15 - 14:00 GMT - Launch Vehicle: M-100. Apogee: 81 km (50 mi). 1982 December 22 - 14:00 GMT - Launch Vehicle: M-100. Apogee: 82 km (50 mi). 1982 December 29 - 14:00 GMT - Launch Vehicle: M-100. Apogee: 83 km (51 mi). 1983 January 5 - 14:00 GMT - Launch Vehicle: M-100. Apogee: 85 km (52 mi). 1983 January 6 - 14:55 GMT - Launch Vehicle: M-100. Apogee: 85 km (52 mi). 1983 January 12 - 14:55 GMT - Launch Vehicle: M-100. Apogee: 84 km (52 mi). 1983 January 19 - 14:00 GMT - Launch Vehicle: M-100. Apogee: 86 km (53 mi). 1983 January 27 - 14:40 GMT - Launch Vehicle: M-100. Apogee: 88 km (54 mi). 1983 February 2 - 14:00 GMT - Launch Vehicle: M-100. Apogee: 86 km (53 mi). 1983 February 9 - 15:15 GMT - Launch Vehicle: M-100. Apogee: 85 km (52 mi). 1983 February 10 - 14:17 GMT - Launch Vehicle: M-100. Apogee: 84 km (52 mi). 1983 February 16 - 14:00 GMT - Launch Vehicle: M-100. Apogee: 81 km (50 mi). 1983 February 23 - 16:20 GMT - Launch Vehicle: M-100. Apogee: 83 km (51 mi). 1983 March 2 - 14:00 GMT - Launch Vehicle: M-100. Apogee: 74 km (45 mi). 1983 March 9 - 14:00 GMT - Launch Vehicle: M-100. Apogee: 83 km (51 mi). 1983 March 16 - 14:00 GMT - Launch Vehicle: M-100. Apogee: 84 km (52 mi). 1983 March 23 - 04:50 GMT - Launch Vehicle: M-100. Ozone intercomparison Aeronomy mission Apogee: 85 km (52 mi). 1983 March 23 - 05:45 GMT - Launch Vehicle: M-100. Ozone intercomparison Aeronomy mission Apogee: 85 km (52 mi). 1983 March 23 - 09:10 GMT - Launch Vehicle: M-100. Ozone intercomparison Aeronomy mission Apogee: 85 km (52 mi). 1983 March 23 - 10:20 GMT - Launch Vehicle: M-100. Ozone intercomparison Aeronomy mission Apogee: 85 km (52 mi). 1983 March 23 - 14:30 GMT - Launch Vehicle: M-100. Ozone intercomparison Aeronomy mission Apogee: 85 km (52 mi). 1983 March 23 - 15:45 GMT - Launch Vehicle: M-100. Ozone intercomparison Aeronomy mission Apogee: 85 km (52 mi). 1983 March 28 - 10:00 GMT - Launch Vehicle: M-100. Ozone intercomparison Aeronomy mission Apogee: 85 km (52 mi). 1983 March 28 - 11:03 GMT - Launch Vehicle: M-100. Ozone intercomparison Aeronomy mission Apogee: 85 km (52 mi). 1983 March 28 - 15:00 GMT - Launch Vehicle: M-100. Ozone intercomparison Aeronomy mission Apogee: 85 km (52 mi). 1983 March 28 - 17:00 GMT - Launch Vehicle: M-100. Ozone intercomparison Aeronomy mission Apogee: 85 km (52 mi). 1983 March 28 - 18:05 GMT - Launch Vehicle: M-100. Ozone intercomparison Aeronomy mission Apogee: 85 km (52 mi). 1983 March 29 - 08:50 GMT - Launch Vehicle: M-100. Ozone intercomparison Aeronomy mission Apogee: 85 km (52 mi). 1983 March 31 - 10:30 GMT - Launch Vehicle: M-100. Ozone intercomparison Aeronomy mission Apogee: 85 km (52 mi). 1983 March 31 - 11:50 GMT - Launch Vehicle: M-100. Ozone intercomparison Aeronomy mission Apogee: 85 km (52 mi). 1983 March 31 - 14:10 GMT - Launch Vehicle: M-100. Ozone intercomparison Aeronomy mission Apogee: 85 km (52 mi). 1983 April 6 - 14:00 GMT - Launch Vehicle: M-100. Apogee: 88 km (54 mi). 1983 April 13 - 14:00 GMT - Launch Vehicle: M-100. Apogee: 84 km (52 mi). 1983 April 21 - 14:00 GMT - Launch Vehicle: M-100. Apogee: 83 km (51 mi). 1983 April 27 - 14:00 GMT - Launch Vehicle: M-100. Apogee: 83 km (51 mi). 1983 May 4 - 14:00 GMT - Launch Vehicle: M-100. Apogee: 84 km (52 mi). 1983 May 11 - 14:00 GMT - Launch Vehicle: M-100. Apogee: 71 km (44 mi). 1983 May 18 - 14:00 GMT - Launch Vehicle: M-100. Apogee: 82 km (50 mi). 1983 May 25 - 14:00 GMT - Launch Vehicle: M-100. Apogee: 82 km (50 mi). 1983 June 1 - 14:00 GMT - Launch Vehicle: M-100. Apogee: 81 km (50 mi). 1983 June 8 - 14:00 GMT - Launch Vehicle: M-100. Apogee: 82 km (50 mi). 1983 June 15 - 14:00 GMT - Launch Vehicle: M-100. Apogee: 86 km (53 mi). 1983 June 22 - 14:00 GMT - Launch Vehicle: M-100. Apogee: 80 km (49 mi). 1983 October 1 - Launch Vehicle: M-100. Apogee: 80 km (49 mi). 1983 October 1 - Launch Vehicle: M-100. Apogee: 80 km (49 mi). 1983 October 1 - Launch Vehicle: M-100. Apogee: 80 km (49 mi). 1983 October 1 - Launch Vehicle: M-100. Apogee: 80 km (49 mi). 1983 November 1 - Launch Vehicle: M-100. Apogee: 80 km (49 mi). 1983 November 1 - Launch Vehicle: M-100. Apogee: 80 km (49 mi). 1983 November 1 - Launch Vehicle: M-100. Apogee: 80 km (49 mi). 1983 November 1 - Launch Vehicle: M-100. Apogee: 80 km (49 mi). 1983 November 1 - Launch Vehicle: M-100. Apogee: 80 km (49 mi). 1983 December 1 - Launch Vehicle: M-100. Apogee: 80 km (49 mi). 1983 December 1 - Launch Vehicle: M-100. Apogee: 80 km (49 mi). 1983 December 1 - Launch Vehicle: M-100. Apogee: 80 km (49 mi). 1983 December 1 - Launch Vehicle: M-100. Apogee: 80 km (49 mi). 1984 January 1 - Launch Vehicle: M-100. Apogee: 80 km (49 mi). 1984 January 1 - Launch Vehicle: M-100. Apogee: 80 km (49 mi). 1984 January 1 - Launch Vehicle: M-100. Apogee: 80 km (49 mi). 1984 January 1 - Launch Vehicle: M-100. Apogee: 80 km (49 mi). 1984 February 1 - Launch Vehicle: M-100. Apogee: 80 km (49 mi). 1984 February 1 - Launch Vehicle: M-100. Apogee: 80 km (49 mi). 1984 February 1 - Launch Vehicle: M-100. Apogee: 80 km (49 mi). 1984 February 1 - Launch Vehicle: M-100. Apogee: 80 km (49 mi). 1984 February 9 - 10:39 GMT - Launch Vehicle: M-100. Gerdien probe Aeronomy mission Agency: ISRO. Apogee: 85 km (52 mi). 1984 March 1 - Launch Vehicle: M-100. Apogee: 80 km (49 mi). 1984 March 1 - Launch Vehicle: M-100. Apogee: 80 km (49 mi). 1984 March 1 - Launch Vehicle: M-100. Apogee: 80 km (49 mi). 1984 March 1 - Launch Vehicle: M-100. Apogee: 80 km (49 mi). 1984 April 1 - Launch Vehicle: M-100. Apogee: 80 km (49 mi). 1984 April 1 - Launch Vehicle: M-100. Apogee: 80 km (49 mi). 1984 April 1 - Launch Vehicle: M-100. Apogee: 80 km (49 mi). 1984 April 1 - Launch Vehicle: M-100. Apogee: 80 km (49 mi). 1984 May 1 - Launch Vehicle: M-100. Apogee: 80 km (49 mi). 1984 May 1 - Launch Vehicle: M-100. Apogee: 80 km (49 mi). 1984 May 1 - Launch Vehicle: M-100. Apogee: 80 km (49 mi). 1984 May 1 - Launch Vehicle: M-100. Apogee: 80 km (49 mi). 1984 May 1 - Launch Vehicle: M-100. Apogee: 80 km (49 mi). 1984 May 23 - 12:48 GMT - Launch Vehicle: RH. RH-200 Eq. Wave Campaign I Meteorological Chaff Meteorological mission Agency: ISRO. Apogee: 60 km (37 mi). 1984 May 23 - 13:54 GMT - Launch Vehicle: RH. RH-200 Eq. Wave Campaign I Meteorological Chaff Meteorological mission Agency: ISRO. Apogee: 61 km (37 mi). 1984 May 25 - 12:30 GMT - Launch Vehicle: RH. RH-200 Eq. Wave Campaign I Meteorological Chaff Meteorological mission Agency: ISRO. Apogee: 68 km (42 mi). 1984 May 27 - 12:34 GMT - Launch Vehicle: RH. RH-200 Eq. Wave Campaign I Meteorological Chaff Meteorological mission Agency: ISRO. Apogee: 64 km (39 mi). 1984 May 29 - 12:37 GMT - Launch Vehicle: RH. RH-200 Eq. Wave Campaign I Meteorological Chaff Meteorological mission Agency: ISRO. Apogee: 66 km (41 mi). 1984 May 31 - 12:30 GMT - Launch Vehicle: RH. RH-200 Eq. Wave Campaign I Meteorological Chaff Meteorological mission Agency: ISRO. Apogee: 69 km (42 mi). 1984 June 1 - Launch Vehicle: M-100. Apogee: 80 km (49 mi). 1984 June 1 - Launch Vehicle: M-100. Apogee: 80 km (49 mi). 1984 June 1 - Launch Vehicle: M-100. Apogee: 80 km (49 mi). 1984 June 1 - Launch Vehicle: M-100. Apogee: 80 km (49 mi). 1984 June 2 - 13:57 GMT - Launch Vehicle: RH. RH-200 Eq. Wave Campaign I Meteorological Chaff Meteorological mission Agency: ISRO. Apogee: 68 km (42 mi). 1984 June 4 - 12:30 GMT - Launch Vehicle: RH. RH-200 Eq. Wave Campaign I Meteorological Chaff Meteorological mission Agency: ISRO. Apogee: 72 km (44 mi). 1984 June 6 - 12:50 GMT - Launch Vehicle: RH. RH-200 Eq. Wave Campaign I Meteorological Chaff Meteorological mission Agency: ISRO. Apogee: 70 km (43 mi). 1984 June 8 - 12:30 GMT - Launch Vehicle: RH. RH-200 Eq. Wave Campaign I Meteorological Chaff Meteorological mission Agency: ISRO. Apogee: 58 km (36 mi). 1984 June 10 - 13:01 GMT - Launch Vehicle: RH. RH-200 Eq. Wave Campaign I Meteorological Chaff Meteorological mission Agency: ISRO. Apogee: 60 km (37 mi). 1984 June 12 - 12:30 GMT - Launch Vehicle: RH. RH-200 Eq. Wave Campaign I Meteorological Chaff Meteorological mission Agency: ISRO. Apogee: 59 km (36 mi). 1984 July 1 - Launch Vehicle: M-100. Apogee: 80 km (49 mi). 1984 July 1 - Launch Vehicle: M-100. Apogee: 80 km (49 mi). 1984 July 1 - Launch Vehicle: M-100. Apogee: 80 km (49 mi). 1984 August 1 - Launch Vehicle: M-100. Apogee: 80 km (49 mi). 1984 August 1 - Launch Vehicle: M-100. Apogee: 80 km (49 mi). 1984 August 1 - Launch Vehicle: M-100. Apogee: 80 km (49 mi). 1984 August 1 - Launch Vehicle: M-100. Apogee: 80 km (49 mi). 1984 August 1 - Launch Vehicle: M-100. Apogee: 80 km (49 mi). 1984 September 1 - Launch Vehicle: M-100. Apogee: 80 km (49 mi). 1984 September 1 - Launch Vehicle: M-100. Apogee: 80 km (49 mi). 1984 December 1 - Launch Vehicle: M-100. Apogee: 80 km (49 mi). 1984 December 1 - Launch Vehicle: M-100. Apogee: 80 km (49 mi). 1984 December 1 - Launch Vehicle: M-100. Apogee: 80 km (49 mi). 1984 December 1 - Launch Vehicle: M-100. Apogee: 80 km (49 mi). 1985 January 1 - Launch Vehicle: M-100. Apogee: 80 km (49 mi). 1985 January 1 - Launch Vehicle: M-100. Apogee: 80 km (49 mi). 1985 January 1 - Launch Vehicle: M-100. Apogee: 80 km (49 mi). 1985 January 1 - Launch Vehicle: M-100. Apogee: 80 km (49 mi). 1985 February 1 - Launch Vehicle: M-100. Apogee: 80 km (49 mi). 1985 February 1 - Launch Vehicle: M-100. Apogee: 80 km (49 mi). 1985 February 1 - Launch Vehicle: M-100. Apogee: 80 km (49 mi). 1985 February 1 - Launch Vehicle: M-100. Apogee: 80 km (49 mi). 1985 April 1 - Launch Vehicle: M-100. Apogee: 80 km (49 mi). 1985 April 1 - Launch Vehicle: M-100. Apogee: 80 km (49 mi). 1985 April 1 - Launch Vehicle: M-100. Apogee: 80 km (49 mi). 1985 April 1 - Launch Vehicle: M-100. Apogee: 80 km (49 mi). 1985 May 1 - Launch Vehicle: M-100. Apogee: 80 km (49 mi). 1985 May 1 - Launch Vehicle: M-100. Apogee: 80 km (49 mi). 1985 May 1 - Launch Vehicle: M-100. Apogee: 80 km (49 mi). 1985 May 1 - Launch Vehicle: M-100. Apogee: 80 km (49 mi). 1985 May 1 - Launch Vehicle: M-100. Apogee: 80 km (49 mi). 1985 June 1 - Launch Vehicle: M-100. Apogee: 80 km (49 mi). 1985 June 1 - Launch Vehicle: M-100. Apogee: 80 km (49 mi). 1985 June 1 - Launch Vehicle: M-100. Apogee: 80 km (49 mi). 1985 June 1 - Launch Vehicle: M-100. Apogee: 80 km (49 mi). 1985 July 2 - 11:43 GMT - Launch Vehicle: M-100. Apogee: 87 km (54 mi). 1985 July 10 - 11:34 GMT - Launch Vehicle: M-100. Apogee: 88 km (54 mi). 1985 July 17 - 11:34 GMT - Launch Vehicle: M-100. Apogee: 85 km (52 mi). 1985 July 18 - 11:55 GMT - Launch Vehicle: M-100. Apogee: 85 km (52 mi). 1985 July 22 - 11:30 GMT - Launch Vehicle: M-100. Apogee: 85 km (52 mi). 1985 July 24 - 11:46 GMT - Launch Vehicle: M-100. Apogee: 81 km (50 mi). 1985 July 26 - 11:30 GMT - Launch Vehicle: M-100. Apogee: 85 km (52 mi). 1985 July 29 - 11:33 GMT - Launch Vehicle: M-100. Apogee: 80 km (49 mi). 1985 July 31 - 11:41 GMT - Launch Vehicle: M-100. Apogee: 81 km (50 mi). 1985 August 2 - 11:30 GMT - Launch Vehicle: M-100. Apogee: 84 km (52 mi). 1985 August 7 - 11:41 GMT - Launch Vehicle: M-100. Apogee: 87 km (54 mi). 1985 August 14 - 11:41 GMT - Launch Vehicle: M-100. Apogee: 87 km (54 mi). 1985 August 22 - 11:42 GMT - Launch Vehicle: M-100. Apogee: 85 km (52 mi). 1985 August 29 - 11:42 GMT - Launch Vehicle: M-100. Apogee: 84 km (52 mi). 1985 September 4 - 11:41 GMT - Launch Vehicle: M-100. Apogee: 81 km (50 mi). 1985 September 11 - 11:31 GMT - Launch Vehicle: M-100. Apogee: 81 km (50 mi). 1985 September 18 - 11:25 GMT - Launch Vehicle: M-100. Apogee: 81 km (50 mi). 1985 October 3 - 11:40 GMT - Launch Vehicle: M-100. Apogee: 87 km (54 mi). 1985 October 9 - 11:45 GMT - Launch Vehicle: M-100. Apogee: 83 km (51 mi). 1985 October 16 - 13:35 GMT - Launch Vehicle: M-100. Apogee: 77 km (47 mi). 1985 October 24 - 12:35 GMT - Launch Vehicle: M-100. Apogee: 80 km (49 mi). 1985 November 3 - 11:52 GMT - Launch Vehicle: M-100. Apogee: 85 km (52 mi). 1985 November 6 - 11:00 GMT - Launch Vehicle: M-100. Apogee: 81 km (50 mi). 1985 November 13 - 11:15 GMT - Launch Vehicle: M-100. Apogee: 82 km (50 mi). 1985 November 20 - 11:54 GMT - Launch Vehicle: M-100. Apogee: 84 km (52 mi). 1985 November 27 - 11:30 GMT - Launch Vehicle: M-100. Apogee: 82 km (50 mi). 1985 December 4 - 11:00 GMT - Launch Vehicle: M-100. Apogee: 83 km (51 mi). 1985 December 11 - 11:00 GMT - Launch Vehicle: M-100. Apogee: 82 km (50 mi). 1985 December 18 - 11:00 GMT - Launch Vehicle: M-100. Apogee: 85 km (52 mi). 1985 December 26 - 11:19 GMT - Launch Vehicle: M-100. Apogee: 83 km (51 mi). 1986 January 1 - 11:16 GMT - Launch Vehicle: M-100. Apogee: 83 km (51 mi). 1986 January 5 - 11:15 GMT - Launch Vehicle: M-100. Apogee: 83 km (51 mi). 1986 January 8 - 12:07 GMT - Launch Vehicle: M-100. M-100B STRATWARM ISRO 8.845 Aeronomy mission Apogee: 85 km (52 mi). 1986 January 15 - 11:15 GMT - Launch Vehicle: M-100. M-100B STRATWARM ISRO 8.846 Aeronomy mission Apogee: 85 km (52 mi). 1986 January 20 - 11:00 GMT - Launch Vehicle: M-100. M-100B STRATWARM ISRO 8.847 Aeronomy mission Apogee: 85 km (52 mi). 1986 January 22 - 11:00 GMT - Launch Vehicle: M-100. M-100B STRATWARM ISRO 8.848 Aeronomy mission Apogee: 83 km (51 mi). 1986 January 24 - 13:30 GMT - Launch Vehicle: M-100. M-100B STRATWARM ISRO 8.849 Aeronomy mission Apogee: 85 km (52 mi). 1986 January 27 - 11:44 GMT - Launch Vehicle: M-100. M-100B STRATWARM ISRO 8.850 Aeronomy mission Apogee: 85 km (52 mi). 1986 January 30 - 11:00 GMT - Launch Vehicle: M-100. M-100B STRATWARM ISRO 8.852 Aeronomy mission Apogee: 82 km (50 mi). 1986 February 5 - 11:06 GMT - Launch Vehicle: M-100. M-100B STRATWARM ISRO 8.854 Aeronomy mission Apogee: 85 km (52 mi). 1986 February 13 - 14:30 GMT - Launch Vehicle: M-100. M-100B STRATWARM ISRO 8.855 Aeronomy mission Apogee: 84 km (52 mi). 1986 February 17 - 11:35 GMT - Launch Vehicle: M-100. M-100B STRATWARM ISRO 8.856 Aeronomy mission Apogee: 85 km (52 mi). 1986 February 20 - 12:00 GMT - Launch Vehicle: M-100. M-100B STRATWARM ISRO 8.858 Aeronomy mission Apogee: 85 km (52 mi). 1986 February 21 - 13:47 GMT - Launch Vehicle: M-100. M-100B STRATWARM ISRO 8.859 Aeronomy mission Apogee: 86 km (53 mi). 1986 February 24 - 13:47 GMT - Launch Vehicle: M-100. M-100B STRATWARM ISRO 8.860 Aeronomy mission Apogee: 85 km (52 mi). 1986 February 27 - 11:36 GMT - Launch Vehicle: M-100. M-100B STRATWARM ISRO 8.861 Aeronomy mission Apogee: 82 km (50 mi). 1986 March 5 - 11:37 GMT - Launch Vehicle: M-100. M-100B STRATWARM ISRO 8.862 Aeronomy mission Apogee: 79 km (49 mi). 1986 March 7 - 05:00 GMT - Launch Vehicle: Belier. D-region ionization comparison Aeronomy mission Agency: ISRO. Apogee: 140 km (80 mi). 1986 March 10 - 04:55 GMT - Launch Vehicle: RH. D-region ionization comparison Aeronomy mission Agency: ISRO. Apogee: 110 km (60 mi). 1986 March 13 - 13:26 GMT - Launch Vehicle: M-100. Apogee: 82 km (50 mi). 1986 March 19 - 11:40 GMT - Launch Vehicle: M-100. Apogee: 81 km (50 mi). 1986 March 27 - 11:37 GMT - Launch Vehicle: M-100. Apogee: 82 km (50 mi). 1986 April 2 - 11:37 GMT - Launch Vehicle: M-100. Apogee: 83 km (51 mi). 1986 April 9 - 11:36 GMT - Launch Vehicle: M-100. Apogee: 82 km (50 mi). 1986 April 17 - 11:35 GMT - Launch Vehicle: M-100. Apogee: 82 km (50 mi). 1986 April 24 - 11:35 GMT - Launch Vehicle: M-100. Apogee: 83 km (51 mi). 1986 April 30 - 11:34 GMT - Launch Vehicle: M-100. Apogee: 81 km (50 mi). 1986 May 7 - 11:36 GMT - Launch Vehicle: M-100. Apogee: 79 km (49 mi). 1986 May 14 - 11:34 GMT - Launch Vehicle: M-100. Apogee: 83 km (51 mi). 1986 May 21 - 11:35 GMT - Launch Vehicle: M-100. Apogee: 87 km (54 mi). 1986 May 22 - 11:54 GMT - Launch Vehicle: M-100. Apogee: 84 km (52 mi). 1986 May 29 - 11:52 GMT - Launch Vehicle: M-100. Apogee: 83 km (51 mi). 1986 June 4 - 11:37 GMT - Launch Vehicle: M-100. Apogee: 84 km (52 mi). 1986 June 11 - 11:34 GMT - Launch Vehicle: M-100. Apogee: 83 km (51 mi). 1986 June 18 - 12:30 GMT - Launch Vehicle: M-100. Apogee: 82 km (50 mi). 1986 June 25 - 11:50 GMT - Launch Vehicle: M-100. Apogee: 90 km (55 mi). 1986 July 2 - 14:42 GMT - Launch Vehicle: M-100. Apogee: 85 km (52 mi). 1986 July 3 - 13:40 GMT - Launch Vehicle: M-100. Apogee: 82 km (50 mi). 1986 July 9 - 11:30 GMT - Launch Vehicle: M-100. Apogee: 85 km (52 mi). 1986 July 16 - 11:45 GMT - Launch Vehicle: M-100. Apogee: 83 km (51 mi). 1986 July 23 - 11:30 GMT - Launch Vehicle: M-100. Apogee: 84 km (52 mi). 1986 July 25 - 11:30 GMT - Launch Vehicle: M-100. Apogee: 85 km (52 mi). 1986 July 29 - 11:30 GMT - Launch Vehicle: M-100. Apogee: 84 km (52 mi). 1986 August 1 - 11:30 GMT - Launch Vehicle: M-100. Apogee: 85 km (52 mi). 1986 August 4 - 12:26 GMT - Launch Vehicle: M-100. Apogee: 80 km (49 mi). 1986 August 6 - 12:35 GMT - Launch Vehicle: M-100. Apogee: 83 km (51 mi). 1986 August 9 - 12:25 GMT - Launch Vehicle: M-100. Apogee: 85 km (52 mi). 1986 August 13 - 11:30 GMT - Launch Vehicle: M-100. Apogee: 89 km (55 mi). 1986 August 20 - 15:15 GMT - Launch Vehicle: M-100. Apogee: 84 km (52 mi). 1986 August 27 - 11:30 GMT - Launch Vehicle: M-100. Apogee: 85 km (52 mi). 1986 September 3 - Launch Vehicle: M-100. Apogee: 85 km (52 mi). 1986 September 10 - 11:30 GMT - Launch Vehicle: M-100. Apogee: 83 km (51 mi). 1986 September 18 - 11:36 GMT - Launch Vehicle: M-100. Apogee: 82 km (50 mi). 1986 September 24 - 11:30 GMT - Launch Vehicle: M-100. Apogee: 80 km (49 mi). 1986 October 1 - Launch Vehicle: M-100. Apogee: 80 km (49 mi). 1986 October 1 - Launch Vehicle: M-100. Apogee: 80 km (49 mi). 1986 October 1 - Launch Vehicle: M-100. Apogee: 80 km (49 mi). 1986 October 1 - Launch Vehicle: M-100. Apogee: 80 km (49 mi). 1986 October 1 - Launch Vehicle: RH. AEROSOL PRECAMP. II Aeronomy mission Agency: ISRO. Apogee: 100 km (60 mi). 1986 October 3 - Launch Vehicle: RH. AEROSOL PRECAMP. II Aeronomy mission Agency: ISRO. Apogee: 100 km (60 mi). 1986 November 1 - Launch Vehicle: M-100. Apogee: 80 km (49 mi). 1986 November 1 - Launch Vehicle: M-100. Apogee: 80 km (49 mi). 1986 November 1 - Launch Vehicle: M-100. Apogee: 80 km (49 mi). 1986 November 1 - Launch Vehicle: M-100. Apogee: 80 km (49 mi). 1986 December 1 - Launch Vehicle: M-100. Apogee: 80 km (49 mi). 1986 December 1 - Launch Vehicle: M-100. Apogee: 80 km (49 mi). 1986 December 1 - Launch Vehicle: M-100. Apogee: 80 km (49 mi). 1987 January 1 - 12:00 GMT - Launch Vehicle: M-100. Apogee: 85 km (52 mi). 1987 January 7 - 11:30 GMT - Launch Vehicle: M-100. Apogee: 85 km (52 mi). 1987 January 21 - 11:34 GMT - Launch Vehicle: M-100. Apogee: 84 km (52 mi). 1987 January 28 - 11:30 GMT - Launch Vehicle: M-100. Apogee: 82 km (50 mi). 1987 February 4 - 11:59 GMT - Launch Vehicle: M-100. Apogee: 81 km (50 mi). 1987 February 11 - 12:12 GMT - Launch Vehicle: M-100. Apogee: 84 km (52 mi). 1987 February 18 - 11:30 GMT - Launch Vehicle: M-100. Apogee: 84 km (52 mi). 1987 February 25 - 12:40 GMT - Launch Vehicle: M-100. Apogee: 83 km (51 mi). 1987 March 4 - 11:30 GMT - Launch Vehicle: M-100. Apogee: 81 km (50 mi). 1987 March 12 - 11:40 GMT - Launch Vehicle: M-100. Apogee: 87 km (54 mi). 1987 March 18 - 12:01 GMT - Launch Vehicle: M-100. Apogee: 89 km (55 mi). 1987 March 25 - 11:30 GMT - Launch Vehicle: M-100. Apogee: 85 km (52 mi). 1987 April 4 - 11:30 GMT - Launch Vehicle: M-100. Apogee: 81 km (50 mi). 1987 April 16 - 11:30 GMT - Launch Vehicle: M-100. Apogee: 81 km (50 mi). 1987 April 22 - 12:02 GMT - Launch Vehicle: M-100. Ion density Apogee: 89 km (55 mi). 1987 April 23 - 11:35 GMT - Launch Vehicle: M-100. Apogee: 85 km (52 mi). 1987 April 29 - 10:40 GMT - Launch Vehicle: M-100. Apogee: 83 km (51 mi). 1987 April 29 - 12:00 GMT - Launch Vehicle: M-100. Ion density Apogee: 83 km (51 mi). 1987 May 6 - 11:38 GMT - Launch Vehicle: M-100. Apogee: 82 km (50 mi). 1987 May 13 - 11:30 GMT - Launch Vehicle: M-100. Apogee: 83 km (51 mi). 1987 May 20 - 12:07 GMT - Launch Vehicle: M-100. Apogee: 83 km (51 mi). 1987 May 27 - 11:56 GMT - Launch Vehicle: M-100. Apogee: 83 km (51 mi). 1987 June 3 - 11:25 GMT - Launch Vehicle: M-100. Apogee: 85 km (52 mi). 1987 June 10 - 11:45 GMT - Launch Vehicle: M-100. Apogee: 81 km (50 mi). 1987 June 17 - 11:45 GMT - Launch Vehicle: M-100. Apogee: 80 km (49 mi). 1987 June 24 - 11:30 GMT - Launch Vehicle: M-100. Apogee: 84 km (52 mi). 1987 July 2 - 11:30 GMT - Launch Vehicle: M-100. Apogee: 82 km (50 mi). 1987 July 8 - 11:30 GMT - Launch Vehicle: M-100. Apogee: 82 km (50 mi). 1987 July 15 - 11:30 GMT - Launch Vehicle: M-100. Apogee: 84 km (52 mi). 1987 July 22 - 11:30 GMT - Launch Vehicle: M-100. Apogee: 86 km (53 mi). 1987 July 24 - 11:30 GMT - Launch Vehicle: M-100. Apogee: 83 km (51 mi). 1987 July 27 - 11:30 GMT - Launch Vehicle: M-100. Apogee: 83 km (51 mi). 1987 July 29 - 11:30 GMT - Launch Vehicle: M-100. Apogee: 84 km (52 mi). 1987 July 31 - 11:30 GMT - Launch Vehicle: M-100. Apogee: 82 km (50 mi). 1987 August 3 - 11:30 GMT - Launch Vehicle: M-100. Apogee: 82 km (50 mi). 1987 August 5 - 11:30 GMT - Launch Vehicle: M-100. Apogee: 80 km (49 mi). 1987 August 12 - 11:30 GMT - Launch Vehicle: M-100. Apogee: 83 km (51 mi). 1987 August 26 - 11:30 GMT - Launch Vehicle: M-100. Apogee: 84 km (52 mi). 1987 September 2 - 11:35 GMT - Launch Vehicle: M-100. Apogee: 85 km (52 mi). 1987 September 23 - 11:32 GMT - Launch Vehicle: M-100. Apogee: 81 km (50 mi). 1987 October 7 - 11:30 GMT - Launch Vehicle: M-100. Apogee: 81 km (50 mi). 1987 October 21 - 11:30 GMT - Launch Vehicle: M-100. Apogee: 85 km (52 mi). 1987 October 28 - 11:45 GMT - Launch Vehicle: M-100. Apogee: 80 km (49 mi). 1987 November 11 - 13:35 GMT - Launch Vehicle: M-100. Apogee: 82 km (50 mi). 1987 December 3 - 03:20 GMT - Launch Vehicle: M-100. Ozone Diurnal Aeronomy mission Apogee: 88 km (54 mi). 1987 December 3 - 14:00 GMT - Launch Vehicle: M-100. Ozone Diurnal Aeronomy mission Apogee: 84 km (52 mi). 1987 December 5 - 03:20 GMT - Launch Vehicle: M-100. Ozone Diurnal Aeronomy mission Apogee: 85 km (52 mi). 1987 December 5 - 08:20 GMT - Launch Vehicle: M-100. Ozone Diurnal Aeronomy mission Apogee: 80 km (49 mi). 1987 December 5 - 09:50 GMT - Launch Vehicle: M-100. Ozone Diurnal Aeronomy mission Apogee: 85 km (52 mi). 1987 December 5 - 14:07 GMT - Launch Vehicle: M-100. Ozone Diurnal Aeronomy mission Apogee: 82 km (50 mi). 1987 December 5 - 16:15 GMT - Launch Vehicle: M-100. Ozone Diurnal Aeronomy mission Apogee: 74 km (45 mi). 1987 December 5 - 17:45 GMT - Launch Vehicle: M-100. Ozone Diurnal Aeronomy mission Apogee: 85 km (52 mi). 1987 December 5 - 18:53 GMT - Launch Vehicle: M-100. Ozone Diurnal Aeronomy mission Apogee: 82 km (50 mi). 1987 December 5 - 22:30 GMT - Launch Vehicle: M-100. Ozone Diurnal Aeronomy mission Apogee: 85 km (52 mi). 1987 December 7 - 09:52 GMT - Launch Vehicle: M-100. Ozone Diurnal Aeronomy mission Apogee: 85 km (52 mi). 1987 December 7 - 14:00 GMT - Launch Vehicle: M-100. Ozone Diurnal Aeronomy mission Apogee: 83 km (51 mi). 1987 December 7 - 16:00 GMT - Launch Vehicle: M-100. Ozone Diurnal Aeronomy mission Apogee: 80 km (49 mi). 1987 December 7 - 18:04 GMT - Launch Vehicle: M-100. Ozone Diurnal Aeronomy mission Apogee: 88 km (54 mi). 1987 December 7 - 22:55 GMT - Launch Vehicle: M-100. Ozone Diurnal Aeronomy mission Apogee: 84 km (52 mi). 1988 January 14 - 11:17 GMT - Launch Vehicle: M-100. Apogee: 85 km (52 mi). 1988 January 27 - 11:25 GMT - Launch Vehicle: M-100. Apogee: 88 km (54 mi). 1988 February 10 - 11:38 GMT - Launch Vehicle: M-100. Apogee: 84 km (52 mi). 1988 March 3 - 11:56 GMT - Launch Vehicle: M-100. Apogee: 87 km (54 mi). 1988 March 9 - 11:37 GMT - Launch Vehicle: M-100. Apogee: 81 km (50 mi). 1988 March 17 - 11:37 GMT - Launch Vehicle: M-100. Apogee: 77 km (47 mi). 1988 March 23 - 11:40 GMT - Launch Vehicle: M-100. Apogee: 81 km (50 mi). 1988 March 30 - 11:37 GMT - Launch Vehicle: M-100. Apogee: 82 km (50 mi). 1988 April 6 - 11:37 GMT - Launch Vehicle: M-100. Apogee: 80 km (49 mi). 1988 April 13 - 11:35 GMT - Launch Vehicle: M-100. Apogee: 78 km (48 mi). 1988 April 21 - 11:35 GMT - Launch Vehicle: M-100. Apogee: 81 km (50 mi). 1988 April 27 - 11:34 GMT - Launch Vehicle: M-100. Apogee: 82 km (50 mi). 1988 May 4 - 11:34 GMT - Launch Vehicle: M-100. Apogee: 82 km (50 mi). 1988 May 11 - 11:42 GMT - Launch Vehicle: M-100. Apogee: 82 km (50 mi). 1988 May 19 - 11:51 GMT - Launch Vehicle: M-100. Apogee: 80 km (49 mi). 1988 May 25 - 11:38 GMT - Launch Vehicle: M-100. Apogee: 82 km (50 mi). 1988 May 31 - Launch Vehicle: RH. RH-200 Daily to Jul 12 Meteorological Chaff Meteorological mission Agency: ISRO. Apogee: 70 km (43 mi). 1988 June 1 - Launch Vehicle: RH. Meteorological Chaff Meteorological mission Agency: ISRO. Apogee: 70 km (43 mi). 1988 June 1 - 11:36 GMT - Launch Vehicle: M-100. Apogee: 81 km (50 mi). 1988 June 2 - Launch Vehicle: RH. Meteorological Chaff Meteorological mission Agency: ISRO. Apogee: 70 km (43 mi). 1988 June 3 - Launch Vehicle: RH. Meteorological Chaff Meteorological mission Agency: ISRO. Apogee: 70 km (43 mi). 1988 June 4 - Launch Vehicle: RH. Meteorological Chaff Meteorological mission Agency: ISRO. Apogee: 70 km (43 mi). 1988 June 5 - Launch Vehicle: RH. Meteorological Chaff Meteorological mission Agency: ISRO. Apogee: 70 km (43 mi). 1988 June 6 - Launch Vehicle: RH. Meteorological Chaff Meteorological mission Agency: ISRO. Apogee: 70 km (43 mi). 1988 June 7 - Launch Vehicle: RH. Meteorological Chaff Meteorological mission Agency: ISRO. Apogee: 70 km (43 mi). 1988 June 8 - Launch Vehicle: RH. Meteorological Chaff Meteorological mission Agency: ISRO. Apogee: 70 km (43 mi). 1988 June 8 - 11:30 GMT - Launch Vehicle: M-100. Apogee: 80 km (49 mi). 1988 June 9 - Launch Vehicle: RH. Meteorological Chaff Meteorological mission Agency: ISRO. Apogee: 70 km (43 mi). 1988 June 10 - Launch Vehicle: RH. Meteorological Chaff Meteorological mission Agency: ISRO. Apogee: 70 km (43 mi). 1988 June 11 - Launch Vehicle: RH. Meteorological Chaff Meteorological mission Agency: ISRO. Apogee: 70 km (43 mi). 1988 June 12 - Launch Vehicle: RH. Meteorological Chaff Meteorological mission Agency: ISRO. Apogee: 70 km (43 mi). 1988 June 13 - Launch Vehicle: RH. Meteorological Chaff Meteorological mission Agency: ISRO. Apogee: 70 km (43 mi). 1988 June 14 - Launch Vehicle: RH. Meteorological Chaff Meteorological mission Agency: ISRO. Apogee: 70 km (43 mi). 1988 June 15 - Launch Vehicle: RH. Meteorological Chaff Meteorological mission Agency: ISRO. Apogee: 70 km (43 mi). 1988 June 15 - 11:45 GMT - Launch Vehicle: M-100. Apogee: 81 km (50 mi). 1988 June 16 - Launch Vehicle: RH. Meteorological Chaff Meteorological mission Agency: ISRO. Apogee: 70 km (43 mi). 1988 June 17 - Launch Vehicle: RH. Meteorological Chaff Meteorological mission Agency: ISRO. Apogee: 70 km (43 mi). 1988 June 18 - Launch Vehicle: RH. Meteorological Chaff Meteorological mission Agency: ISRO. Apogee: 70 km (43 mi). 1988 June 19 - Launch Vehicle: RH. Meteorological Chaff Meteorological mission Agency: ISRO. Apogee: 70 km (43 mi). 1988 June 20 - Launch Vehicle: RH. Meteorological Chaff Meteorological mission Agency: ISRO. Apogee: 70 km (43 mi). 1988 June 21 - Launch Vehicle: RH. Meteorological Chaff Meteorological mission Agency: ISRO. Apogee: 70 km (43 mi). 1988 June 22 - Launch Vehicle: RH. Meteorological Chaff Meteorological mission Agency: ISRO. Apogee: 70 km (43 mi). 1988 June 22 - 11:48 GMT - Launch Vehicle: M-100. Apogee: 81 km (50 mi). 1988 June 23 - Launch Vehicle: RH. Meteorological Chaff Meteorological mission Agency: ISRO. Apogee: 70 km (43 mi). 1988 June 24 - Launch Vehicle: RH. Meteorological Chaff Meteorological mission Agency: ISRO. Apogee: 70 km (43 mi). 1988 June 25 - Launch Vehicle: RH. Meteorological Chaff Meteorological mission Agency: ISRO. Apogee: 70 km (43 mi). 1988 June 26 - Launch Vehicle: RH. Meteorological Chaff Meteorological mission Agency: ISRO. Apogee: 70 km (43 mi). 1988 June 27 - Launch Vehicle: RH. Meteorological Chaff Meteorological mission Agency: ISRO. Apogee: 70 km (43 mi). 1988 June 28 - Launch Vehicle: RH. Meteorological Chaff Meteorological mission Agency: ISRO. Apogee: 70 km (43 mi). 1988 June 29 - Launch Vehicle: RH. Meteorological Chaff Meteorological mission Agency: ISRO. Apogee: 70 km (43 mi). 1988 June 29 - 11:35 GMT - Launch Vehicle: M-100. Apogee: 80 km (49 mi). 1988 June 30 - Launch Vehicle: RH. Meteorological Chaff Meteorological mission Agency: ISRO. Apogee: 70 km (43 mi). 1988 July 1 - Launch Vehicle: RH. Meteorological Chaff Meteorological mission Agency: ISRO. Apogee: 70 km (43 mi). 1988 July 2 - Launch Vehicle: RH. Meteorological Chaff Meteorological mission Agency: ISRO. Apogee: 70 km (43 mi). 1988 July 3 - Launch Vehicle: RH. Meteorological Chaff Meteorological mission Agency: ISRO. Apogee: 70 km (43 mi). 1988 July 4 - Launch Vehicle: RH. Meteorological Chaff Meteorological mission Agency: ISRO. Apogee: 70 km (43 mi). 1988 July 5 - Launch Vehicle: RH. Meteorological Chaff Meteorological mission Agency: ISRO. Apogee: 70 km (43 mi). 1988 July 6 - Launch Vehicle: RH. Meteorological Chaff Meteorological mission Agency: ISRO. Apogee: 70 km (43 mi). 1988 July 6 - 11:30 GMT - Launch Vehicle: M-100. Apogee: 81 km (50 mi). 1988 July 7 - Launch Vehicle: RH. Meteorological Chaff Meteorological mission Agency: ISRO. Apogee: 70 km (43 mi). 1988 July 8 - Launch Vehicle: RH. Meteorological Chaff Meteorological mission Agency: ISRO. Apogee: 70 km (43 mi). 1988 July 9 - Launch Vehicle: RH. Meteorological Chaff Meteorological mission Agency: ISRO. Apogee: 70 km (43 mi). 1988 July 10 - Launch Vehicle: RH. Meteorological Chaff Meteorological mission Agency: ISRO. Apogee: 70 km (43 mi). 1988 July 11 - Launch Vehicle: RH. Meteorological Chaff Meteorological mission Agency: ISRO. Apogee: 70 km (43 mi). 1988 July 12 - Launch Vehicle: RH. Meteorological Chaff Meteorological mission Agency: ISRO. Apogee: 70 km (43 mi). 1988 July 13 - 11:40 GMT - Launch Vehicle: M-100. Apogee: 81 km (50 mi). 1988 July 20 - 11:40 GMT - Launch Vehicle: M-100. Apogee: 81 km (50 mi). 1988 July 27 - 11:30 GMT - Launch Vehicle: M-100. Apogee: 80 km (49 mi). 1988 August 3 - 11:30 GMT - Launch Vehicle: M-100. Apogee: 80 km (49 mi). 1988 August 10 - 11:59 GMT - Launch Vehicle: M-100. Apogee: 81 km (50 mi). 1988 August 17 - 11:30 GMT - Launch Vehicle: M-100. Apogee: 80 km (49 mi). 1988 August 24 - 12:25 GMT - Launch Vehicle: M-100. Apogee: 83 km (51 mi). 1988 August 31 - 11:30 GMT - Launch Vehicle: M-100. Apogee: 81 km (50 mi). 1988 September 7 - 11:41 GMT - Launch Vehicle: M-100. Apogee: 86 km (53 mi). 1988 September 10 - 02:30 GMT - Launch Vehicle: M-100. Apogee: 87 km (54 mi). 1988 September 10 - 12:15 GMT - Launch Vehicle: M-100. Apogee: 87 km (54 mi). 1988 September 10 - 13:15 GMT - Launch Vehicle: M-100. Apogee: 83 km (51 mi). 1988 September 14 - 11:28 GMT - Launch Vehicle: M-100. Apogee: 81 km (50 mi). 1988 September 21 - 11:27 GMT - Launch Vehicle: M-100. Apogee: 84 km (52 mi). 1988 September 28 - 11:39 GMT - Launch Vehicle: M-100. Apogee: 80 km (49 mi). 1988 October 5 - 11:17 GMT - Launch Vehicle: M-100. Apogee: 80 km (49 mi). 1988 October 12 - 11:11 GMT - Launch Vehicle: M-100. Apogee: 83 km (51 mi). 1988 October 19 - 11:07 GMT - Launch Vehicle: M-100. Apogee: 83 km (51 mi). 1988 October 26 - 11:03 GMT - Launch Vehicle: M-100. Apogee: 83 km (51 mi). 1988 November 2 - 11:01 GMT - Launch Vehicle: M-100. Apogee: 81 km (50 mi). 1988 November 10 - 10:59 GMT - Launch Vehicle: M-100. Apogee: 81 km (50 mi). 1988 November 16 - 10:57 GMT - Launch Vehicle: M-100. Apogee: 83 km (51 mi). 1988 November 23 - 11:00 GMT - Launch Vehicle: M-100. Apogee: 78 km (48 mi). 1988 November 30 - 10:57 GMT - Launch Vehicle: M-100. Apogee: 81 km (50 mi). 1988 December 7 - 10:01 GMT - Launch Vehicle: M-100. Apogee: 84 km (52 mi). 1988 December 14 - 11:01 GMT - Launch Vehicle: M-100. Apogee: 81 km (50 mi). 1988 December 21 - 11:01 GMT - Launch Vehicle: M-100. Apogee: 82 km (50 mi). 1988 December 28 - 11:08 GMT - Launch Vehicle: M-100. Apogee: 82 km (50 mi). 1989 January 9 - 11:25 GMT - Launch Vehicle: M-100. Apogee: 83 km (51 mi). 1989 January 11 - 11:16 GMT - Launch Vehicle: M-100. Apogee: 77 km (47 mi). 1989 January 16 - 11:52 GMT - Launch Vehicle: M-100. Apogee: 81 km (50 mi). 1989 January 18 - 11:27 GMT - Launch Vehicle: M-100. Apogee: 81 km (50 mi). 1989 January 23 - 11:00 GMT - Launch Vehicle: M-100. Apogee: 81 km (50 mi). 1989 January 23 - 12:38 GMT - Launch Vehicle: M-100. Apogee: 81 km (50 mi). 1989 January 25 - 11:46 GMT - Launch Vehicle: M-100. Apogee: 84 km (52 mi). 1989 January 25 - 13:16 GMT - Launch Vehicle: M-100. Apogee: 81 km (50 mi). 1989 February 1 - 11:33 GMT - Launch Vehicle: M-100. Apogee: 83 km (51 mi). 1989 February 6 - 11:31 GMT - Launch Vehicle: M-100. Apogee: 83 km (51 mi). 1989 February 8 - 11:31 GMT - Launch Vehicle: M-100. Apogee: 80 km (49 mi). 1989 February 13 - 11:33 GMT - Launch Vehicle: M-100. Apogee: 80 km (49 mi). 1989 February 15 - 11:41 GMT - Launch Vehicle: M-100. Apogee: 83 km (51 mi). 1989 May 4 - 11:33 GMT - Launch Vehicle: M-100. Apogee: 77 km (47 mi). 1989 May 10 - 11:20 GMT - Launch Vehicle: M-100. Apogee: 83 km (51 mi). 1989 May 17 - 11:02 GMT - Launch Vehicle: M-100. Apogee: 82 km (50 mi). 1989 May 24 - 11:52 GMT - Launch Vehicle: M-100. Apogee: 81 km (50 mi). 1989 May 31 - 11:10 GMT - Launch Vehicle: M-100. Apogee: 81 km (50 mi). 1989 June 1 - 13:06 GMT - Launch Vehicle: M-100. Apogee: 79 km (49 mi). 1989 June 7 - 11:30 GMT - Launch Vehicle: M-100. Apogee: 79 km (49 mi). 1989 June 14 - 11:10 GMT - Launch Vehicle: M-100. Apogee: 79 km (49 mi). 1989 June 21 - 11:10 GMT - Launch Vehicle: M-100. Apogee: 77 km (47 mi). 1989 June 28 - 11:10 GMT - Launch Vehicle: M-100. Apogee: 79 km (49 mi). 1989 July 5 - 11:26 GMT - Launch Vehicle: M-100. Apogee: 81 km (50 mi). 1989 July 12 - 11:10 GMT - Launch Vehicle: M-100. Apogee: 86 km (53 mi). 1989 July 20 - 13:23 GMT - Launch Vehicle: M-100. Apogee: 82 km (50 mi). 1989 July 26 - 11:36 GMT - Launch Vehicle: M-100. Apogee: 81 km (50 mi). 1989 August 2 - 11:22 GMT - Launch Vehicle: M-100. Apogee: 72 km (44 mi). 1989 August 9 - 11:10 GMT - Launch Vehicle: M-100. Apogee: 80 km (49 mi). 1989 August 16 - 11:10 GMT - Launch Vehicle: M-100. Apogee: 81 km (50 mi). 1989 August 23 - 11:10 GMT - Launch Vehicle: M-100. Apogee: 81 km (50 mi). 1989 August 30 - 10:10 GMT - Launch Vehicle: M-100. Apogee: 80 km (49 mi). 1989 September 6 - 11:10 GMT - Launch Vehicle: M-100. Apogee: 79 km (49 mi). 1989 September 13 - 11:45 GMT - Launch Vehicle: M-100. Apogee: 76 km (47 mi). 1989 September 20 - 11:20 GMT - Launch Vehicle: M-100. Apogee: 81 km (50 mi). 1989 September 27 - 11:15 GMT - Launch Vehicle: M-100. Apogee: 81 km (50 mi). 1989 October 4 - 11:10 GMT - Launch Vehicle: M-100. Apogee: 78 km (48 mi). 1989 October 11 - 11:10 GMT - Launch Vehicle: M-100. Apogee: 78 km (48 mi). 1989 October 25 - 11:18 GMT - Launch Vehicle: M-100. Apogee: 83 km (51 mi). 1989 November 8 - 11:18 GMT - Launch Vehicle: M-100. Apogee: 77 km (47 mi). 1989 November 23 - 10:40 GMT - Launch Vehicle: M-100. Apogee: 82 km (50 mi). 1989 December 6 - 11:18 GMT - Launch Vehicle: M-100. Apogee: 80 km (49 mi). 1989 December 20 - 11:18 GMT - Launch Vehicle: M-100. Apogee: 80 km (49 mi). 1990 January 3 - 11:10 GMT - Launch Vehicle: M-100. Apogee: 80 km (49 mi). 1990 January 10 - 11:10 GMT - Launch Vehicle: M-100. Apogee: 80 km (49 mi). 1990 January 15 - 11:10 GMT - Launch Vehicle: M-100. Apogee: 80 km (49 mi). 1990 January 17 - 11:10 GMT - Launch Vehicle: M-100. DYANA DTM2 Apogee: 80 km (49 mi). 1990 January 19 - 11:10 GMT - Launch Vehicle: M-100. DYANA DTM3 Apogee: 80 km (49 mi). 1990 January 22 - 11:10 GMT - Launch Vehicle: M-100. Apogee: 80 km (49 mi). 1990 January 24 - 11:10 GMT - Launch Vehicle: M-100. DYANA DTM5 Apogee: 77 km (47 mi). 1990 January 26 - 11:10 GMT - Launch Vehicle: M-100. DYANA DTM6 Apogee: 77 km (47 mi). 1990 February 1 - 12:05 GMT - Launch Vehicle: M-100. DYANA DTM7 Apogee: 80 km (49 mi). 1990 February 2 - 13:05 GMT - Launch Vehicle: M-100. DYANA DTM8 Apogee: 75 km (46 mi). 1990 February 5 - 11:45 GMT - Launch Vehicle: M-100. Apogee: 83 km (51 mi). 1990 February 7 - 14:10 GMT - Launch Vehicle: M-100. DYANA DTM10 Apogee: 80 km (49 mi). 1990 February 8 - 11:10 GMT - Launch Vehicle: M-100. Apogee: 80 km (49 mi). 1990 February 9 - 11:10 GMT - Launch Vehicle: M-100. DYANA DTM11 Apogee: 80 km (49 mi). 1990 February 12 - 12:50 GMT - Launch Vehicle: M-100. DYANA DTM12 Apogee: 80 km (49 mi). 1990 February 14 - 11:45 GMT - Launch Vehicle: M-100. DYANA DTM13 Apogee: 85 km (52 mi). 1990 February 16 - 11:10 GMT - Launch Vehicle: M-100. DYANA DTM14 Apogee: 87 km (54 mi). 1990 February 19 - 11:40 GMT - Launch Vehicle: M-100. DYANA DTM15 Apogee: 81 km (50 mi). 1990 February 21 - 11:22 GMT - Launch Vehicle: M-100. DYANA DTM16 Apogee: 86 km (53 mi). 1990 February 23 - 11:10 GMT - Launch Vehicle: M-100. DYANA DTM17 Apogee: 85 km (52 mi). 1990 February 26 - 11:35 GMT - Launch Vehicle: M-100. DYANA DTM18 Apogee: 85 km (52 mi). 1990 February 28 - 11:10 GMT - Launch Vehicle: M-100. DYANA DTM19 Apogee: 80 km (49 mi). 1990 March 2 - 11:35 GMT - Launch Vehicle: M-100. DYANA DTM20 Apogee: 85 km (52 mi). 1990 March 7 - 11:10 GMT - Launch Vehicle: M-100. DYANA DTM21 Apogee: 79 km (49 mi). 1990 March 12 - 14:00 GMT - Launch Vehicle: M-100. DYANA DTM22 Apogee: 80 km (49 mi). 1990 September 1 - 12:05 GMT - Launch Vehicle: M-100. Apogee: 80 km (49 mi). 1991 - Launch Vehicle: M-100. Apogee: 79 km (49 mi). 1991 - Launch Vehicle: M-100. Apogee: 79 km (49 mi). 1991 - Launch Vehicle: M-100. Apogee: 79 km (49 mi). 1991 - Launch Vehicle: M-100. Apogee: 79 km (49 mi). 1991 - Launch Vehicle: M-100. Apogee: 79 km (49 mi). 1991 - Launch Vehicle: M-100. Apogee: 79 km (49 mi). 1991 - Launch Vehicle: M-100. Apogee: 79 km (49 mi). 1991 - Launch Vehicle: M-100. Apogee: 79 km (49 mi). 1991 - Launch Vehicle: M-100. Apogee: 79 km (49 mi). 1991 - Launch Vehicle: M-100. Apogee: 79 km (49 mi). 1991 - Launch Vehicle: M-100. Apogee: 79 km (49 mi). 1991 - Launch Vehicle: M-100. Apogee: 79 km (49 mi). 1991 - Launch Vehicle: M-100. Apogee: 79 km (49 mi). 1991 - Launch Vehicle: M-100. Apogee: 79 km (49 mi). 1991 - Launch Vehicle: M-100. Apogee: 79 km (49 mi). 1991 - Launch Vehicle: M-100. Apogee: 79 km (49 mi). 1991 - Launch Vehicle: M-100. Apogee: 79 km (49 mi). 1991 - Launch Vehicle: M-100. Apogee: 79 km (49 mi). 1991 - Launch Vehicle: M-100. Apogee: 79 km (49 mi). 1991 - Launch Vehicle: M-100. Apogee: 79 km (49 mi). 1991 - Launch Vehicle: M-100. Apogee: 79 km (49 mi). 1993 - Launch Vehicle: M-100. M-100B Meteo Apogee: 79 km (49 mi). 1993 - Launch Vehicle: M-100. M-100B Meteo Apogee: 79 km (49 mi). 1993 - Launch Vehicle: M-100. M-100B Meteo Apogee: 79 km (49 mi). 1993 - Launch Vehicle: M-100. M-100B Meteo Apogee: 79 km (49 mi). 1993 - Launch Vehicle: M-100. M-100B Meteo Apogee: 79 km (49 mi). 1993 - Launch Vehicle: M-100. M-100B Meteo Apogee: 79 km (49 mi). 1993 September 1 - Launch Vehicle: M-100. TERLS M100 #1162 Apogee: 80 km (49 mi). 2002 August 12 - 13:48 GMT - Launch Vehicle: RH. Middle Atmosphere Aeronomy mission Agency: ISRO. Apogee: 70 km (43 mi). 2002 November 21 - Launch Vehicle: RH. Middle Atmosphere Aeronomy mission Agency: ISRO. Apogee: 70 km (43 mi). 2003 November 21 - 10:30 GMT - Launch Vehicle: RH. Anniversary Aeronomy mission Agency: ISRO. Apogee: 70 km (43 mi). 2004 September 10 - 11:00 GMT - Launch Vehicle: RH. Middle Atmosphere Aeronomy mission Agency: ISRO. Apogee: 70 km (43 mi). 2004 September 24 - Launch Vehicle: RH. Middle Atmosphere Aeronomy mission Agency: ISRO. Apogee: 70 km (43 mi). 2004 October 6 - Launch Vehicle: RH. Middle Atmosphere Aeronomy mission Agency: ISRO. Apogee: 74 km (45 mi). Contact us with any corrections, additions, or comments. Conditions for use of drawings, pictures, or other materials from this site.. To contact astronauts or cosmonauts. © Mark Wade, 1997 - 2008 except where otherwise noted. |
