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1953 - Launch Site: Hammaguira. Launch Complex: Bechar. Launch Pad: -. Launch Vehicle: Veronique. LV Configuration: Veronique N10.

  • Test mission Nation: France. Agency: FR. Apogee: 45 km (27 mi).

1955 - 15:58 GMT - Launch Site: Holloman. Launch Complex: A. Launch Pad: -. Launch Vehicle: Aerobee. Model: Aerobee Hi. LV Configuration: Aerobee Hi USAF 55.
  • AJ11-6 engine test Nation: USA. Agency: USAF. Apogee: 198 km (123 mi).

    First launcing of USAF Aerobee-Hi sounding rocket. Rocket test, 98 kg payload. Launched at 0858 local time. Reached 198 km.

1959 - 01:05 GMT - Launch Site: Holloman. Launch Complex: A. Launch Pad: -. Launch Vehicle: Aerobee. Model: Aerobee 150. LV Configuration: Aerobee 150 AA3.181C.
  • Ionosphere mission Nation: USA. Agency: USAF. Apogee: 235 km (146 mi).

1960 -
  • SAINT System Development Requirement issued. Nation: USA. Spacecraft: SAINT, SAINT II.

    It also allowed follow-on manned systems to be pursued.

1960 - 10:35 GMT - Launch Site: Woomera. Launch Complex: LA2. Launch Pad: LA2 SL. Launch Vehicle: Skylark. Model: Skylark 2. LV Configuration: Skylark-2 SL62.
  • Grenades / Chaff Aeronomy mission Nation: Australia. Agency: WRE/RAE. Apogee: 141 km (87 mi).

1960 - 15:00 GMT - Launch Site: Eglin. Launch Complex: -. Launch Pad: -. Launch Vehicle: Aerobee. Model: Aerobee 150. LV Configuration: Aerobee 150 AA3.283C.
  • Magnetometer Fields mission Nation: USA. Agency: USAF. Apogee: 245 km (152 mi).

1960 - 20:55 GMT - Launch Site: Cape Canaveral. Launch Complex: LC15. Launch Pad: -. Launch Vehicle: Titan. Model: Titan 1. LV Configuration: Titan I G-6.
  • RVX-4 test Nation: USA. Agency: USAF. Apogee: 1,000 km (600 mi).

1961 - Launch Site: Baikonur. Launch Complex: LC41/4. Launch Pad: LC41/pad?. Launch Vehicle: R-16. LV Configuration: R-16 6L-11T. FAILURE: Failure.
  • Test mission Nation: USSR. Agency: RVSN. Apogee: 0 km ( mi).

1961 - 00:12 GMT - Launch Site: Wallops Island. Launch Complex: -. Launch Pad: -. Launch Vehicle: Asp. Model: Nike Asp. LV Configuration: Nike Asp NASA 03.06CA. FAILURE: Failure.
  • Sodium release Aeronomy mission Nation: USA. Agency: NASA. Apogee: 180 km (110 mi).

1961 - 02:26 GMT - Launch Site: Baikonur. Launch Complex: LC51. Launch Pad: -. Launch Vehicle: R-9. Model: Romashka. LV Configuration: R-9 No. E10309.
  • State trials missile test Nation: USSR. Agency: RVSN. Apogee: 1,160 km (720 mi).

1961 - 09:34 GMT - Launch Site: Wallops Island. Launch Complex: -. Launch Pad: -. Launch Vehicle: Asp. Model: Nike Asp. LV Configuration: Nike Asp NASA 03.07CA. FAILURE: Failure.
  • Sodium release Aeronomy mission Nation: USA. Agency: NASA. Apogee: 200 km (120 mi).

1961 - 09:39 GMT - Launch Site: Wallops Island. Launch Complex: -. Launch Pad: -. Launch Vehicle: Asp. Model: Nike Asp. LV Configuration: Nike Asp NASA 03.08CA.
  • Sodium release Aeronomy mission Nation: USA. Agency: NASA. Apogee: 165 km (102 mi).

1961 - 12:00 GMT - Launch Site: Wallops Island. Launch Complex: -. Launch Pad: -. Launch Vehicle: Aerobee. Model: Aerobee 150A. LV Configuration: Aerobee 150A NASA 04.39NP.
  • LeRC LH2 test Technology test Nation: USA. Agency: NASA. Apogee: 154 km (95 mi).

1961 - 18:05 GMT - Launch Site: Hidden Hills DZ. Launch Complex: -. Launch Pad: 36.1 N x 116.0 W. Launch Vehicle: X-15. LV Configuration: X-15 2-15-29. FAILURE: Three hardware problems during flight.
  • X-15A Mach 4, Aero test Nation: USA. Agency: NASA/USAF. Apogee: 32 km (19 mi).

    Maximum Speed - 4946 kph. Maximum Altitude - 32000 m.

1964 - 06:15 GMT - Launch Site: Johnston Island. Launch Complex: LE2. Launch Pad: -. Launch Vehicle: Delta. Model: Thor DSV-2J. LV Configuration: Thor DSV-2J 290 (20003).
  • AFP-437 combat training interceptor mission Nation: USA. Agency: USAF 10ADS. Apogee: 778 km (483 mi).

1964 - 18:50 GMT - Launch Site: Vandenberg. Launch Complex: SLC2E. Launch Pad: -. Launch Vehicle: Delta. Model: Thor Ablestar. LV Configuration: Thor Ablestar-2 379 AB014. FAILURE: Failure.
  • Transit 5BN-3 Nation: USA. Program: Transit. Mass: 75 kg (165 lb). Class: Navigation. Spacecraft: Transit. Agency: U.S. Navy. COSPAR: F640421A. Decay Date: 1964-04-21.

    Carried SNAP-9A nuclear power source. After this launch failure it was decided that operational Transits would be solar-powered only.

  • Transit 5E-4 Nation: USA. Program: Transit. Class: Earth. Type: Magnetosphere. Spacecraft: Transit. Agency: U.S. Navy. COSPAR: F640421B.

    Radiation monitoring.

1964 - 23:56 GMT - Launch Site: Fort Churchill. Launch Complex: -. Launch Pad: -. Launch Vehicle: Black Brant. Model: Black Brant 3. LV Configuration: Black Brant III FF-3-09.
  • Test mission Nation: Canada. Agency: NRCC. Apogee: 150 km (90 mi).

1965 - Launch Vehicle: Titan. Model: Titan 2.
  • The Combined Systems Acceptance Test (CSAT) of Gemini launch vehicle (GLV) 5 was conducted in the vertical test facility at Martin-Baltimore. Nation: USA. Flight: Gemini 5.

    Four earlier CSAT attempts (April 15-20) were marred by numerous minor anomalies. The vehicle acceptance team inspection began April 26 and concluded April 30, with GLV-5 found acceptable. The vehicle was removed from the test cell May 7-8, formally accepted by the Air Force May 15, and shipped to Cape Kennedy. Stage I arrived at the Cape on May 17 and stage II on May 19.

1965 - 11:02 GMT - Launch Site: Woomera. Launch Complex: LA5B. Launch Pad: LA5B?. Launch Vehicle: Black Knight. Model: Black Knight 301/C2. LV Configuration: Black Knight-301/C2 BK.21.
  • Dazzle re-entry vehicle test Nation: UK. Agency: RAE. Apogee: 651 km (404 mi).

1966 - Launch Site: ETR Launch Area. Launch Complex: -. Launch Pad: -. Launch Vehicle: Polaris. Model: Polaris A3. LV Configuration: Polaris A3P-437.
  • Operational test Nation: USA. Agency: USN. Apogee: 1,000 km (600 mi).

1966 - Launch Site: Baikonur. Launch Complex: -. Launch Pad: -. Launch Vehicle: UR-100. FAILURE: Failure.
  • Joint flight trials launch Nation: USSR. Agency: RVSN. Apogee: 0 km ( mi).

1966 - 00:06 GMT - Launch Site: Woomera. Launch Complex: LA2. Launch Pad: LA2 SL. Launch Vehicle: Skylark. Model: Skylark 2. LV Configuration: Skylark 2 SL583.
  • Test mission Nation: Australia. Agency: WRE/RAE. Apogee: 193 km (119 mi).

1966 - 02:10 GMT - Launch Site: Tonopah. Launch Complex: -. Launch Pad: -. Launch Vehicle: Apache. Model: Nike Apache.
  • Sandia 154-75 Aeronomy mission Nation: USA. Agency: Sandia. Apogee: 160 km (90 mi).

1966 - 11:25 GMT - Launch Site: White Sands. Launch Complex: LC35. Launch Pad: -. Launch Vehicle: Aerobee. Model: Aerobee 150. LV Configuration: Aerobee 150 NASA 04.165UA.
  • JHU UVT F1 (Venus) Ultraviolet astronomy mission Nation: USA. Agency: NASA. Apogee: 154 km (95 mi).

1966 - 16:00 GMT - Launch Site: ETR Launch Area. Launch Complex: -. Launch Pad: -. Launch Vehicle: Polaris. Model: Polaris A3. LV Configuration: Polaris A3P-440.
  • Operational test Nation: USA. Agency: USN. Apogee: 1,000 km (600 mi).

1966 - 16:30 GMT - Launch Site: ETR Launch Area. Launch Complex: -. Launch Pad: -. Launch Vehicle: Polaris. Model: Polaris A3. LV Configuration: Polaris A3P-431.
  • Operational test Nation: USA. Agency: USN. Apogee: 1,000 km (600 mi).

1967 - Launch Site: Vandenberg. Launch Complex: LF03. Launch Pad: -. Launch Vehicle: Minuteman 1. Model: Minuteman 1B. LV Configuration: Minuteman 1B 1296.
  • Follow-on operational missile test Nation: USA. Agency: SAC 1STRAD. Apogee: 1,300 km (800 mi).

1967 - Launch Site: Vandenberg. Launch Complex: LF22. Launch Pad: -. Launch Vehicle: Minuteman 2. LV Configuration: Minuteman 2 2137.
  • ST Olympic Trials 1 operational test launch Nation: USA. Agency: SAC 1STRAD. Apogee: 1,300 km (800 mi).

1968 -
  • L1 on schedule; N1 in trouble. Nation: USSR. Program: Lunar L1, Lunar L3. Spacecraft: Soyuz 7K-L1.

    This was a reserve day in the L1 countdown, in case of problems in preparation. However all is on schedule for the launch. The same cannot be said for the N1. There are many delays. Mishin promised the first N1 rollout in the first half of March, but it is still in the assembly building, with no end in sight of preparations. The weather at the cosmodrome is -5 deg at night, clear pleasant days. The Hotel Kosmonavt was finished on 15 April. Although it has all of its furniture, it was not completely painted before the furniture was moved in!

1968 - 04:20 GMT - Launch Site: Baikonur. Launch Complex: LC1. Launch Pad: LC1 or LC31. Launch Vehicle: Soyuz. Model: Molniya 8K78M.
  • Molniya 1-08 Nation: USSR. Program: Molniya. Payload: Molniya-1. Mass: 1,600 kg (3,500 lb). Class: Communications. Spacecraft: Molniya-1. Agency: MOM. Perigee: 405 km (251 mi). Apogee: 40,099 km (24,916 mi). Inclination: 64.00 deg. Period: 720.80 min. COSPAR: 1968-035A. USAF Sat Cat: 3209. Decay Date: 1974-01-29.

    Operation of a system of long range telephone-telegraph radiocommunication, and transmission of USSR Central Television programmes to the stations of the Orbita network.

1969 - Launch Vehicle: Shuttle.
  • Space Shuttle Task Group formed Nation: USA. Program: STS.

    The Director of Apollo Test in the NASA Hq. Apollo Program Office, LeRoy E. Day, was detailed to head the MSF Space Shuttle Task Group. The group would provide NASA with material for a report on the Space Shuttle to the President's Space Task Group.

1969 - 13:06 GMT - Launch Site: Kapustin Yar. Launch Complex: V-2. Launch Pad: -. Launch Vehicle: MR-12.
  • Aeronomy/Plasma mission Nation: USSR. Agency: AN SSSR. Apogee: 173 km (107 mi).

1969 - 15:26 GMT - Launch Site: Kapustin Yar. Launch Complex: V-2. Launch Pad: -. Launch Vehicle: MR-12.
  • Solar Extreme ultraviolet mission Nation: USSR. Agency: AN SSSR. Apogee: 176 km (109 mi).

1970 - Launch Site: ETR Launch Area. Launch Complex: -. Launch Pad: -. Launch Vehicle: Polaris. Model: Polaris A2.
  • Operational missile test Nation: USA. Agency: USN. Apogee: 1,000 km (600 mi).

1970 - Launch Site: ETR Launch Area. Launch Complex: -. Launch Pad: -. Launch Vehicle: Polaris. Model: Polaris A2.
  • Operational missile test Nation: USA. Agency: USN. Apogee: 1,000 km (600 mi).

1970 - Launch Site: ETR Launch Area. Launch Complex: -. Launch Pad: -. Launch Vehicle: Polaris. Model: Polaris A2.
  • Operational missile test Nation: USA. Agency: USN. Apogee: 1,000 km (600 mi).

1970 - Launch Site: ETR Launch Area. Launch Complex: -. Launch Pad: -. Launch Vehicle: Polaris. Model: Polaris A2.
  • Operational missile test Nation: USA. Agency: USN. Apogee: 1,000 km (600 mi).

1970 - Launch Site: ETR Launch Area. Launch Complex: -. Launch Pad: -. Launch Vehicle: Polaris. Model: Polaris A2.
  • Operational missile test Nation: USA. Agency: USN. Apogee: 1,000 km (600 mi).

1970 - Launch Site: ETR Launch Area. Launch Complex: -. Launch Pad: -. Launch Vehicle: Polaris. Model: Polaris A2.
  • Operational missile test Nation: USA. Agency: USN. Apogee: 1,000 km (600 mi).

1970 - Launch Site: ETR Launch Area. Launch Complex: -. Launch Pad: -. Launch Vehicle: Polaris. Model: Polaris A2.
  • Operational missile test Nation: USA. Agency: USN. Apogee: 1,000 km (600 mi).

1970 - Launch Site: Vandenberg. Launch Complex: LF24. Launch Pad: -. Launch Vehicle: Minuteman 2. LV Configuration: Minuteman 2 2474.
  • OT GT48F operational test launch Nation: USA. Agency: USAF SAC. Apogee: 1,300 km (800 mi).

1970 - 06:01 GMT - Launch Site: Kapustin Yar. Launch Complex: V-2. Launch Pad: -. Launch Vehicle: MR-12.
  • Ionosphere mission Nation: USSR. Apogee: 175 km (108 mi).

1970 - 20:42 GMT - Launch Site: South Uist. Launch Complex: -. Launch Pad: -. Launch Vehicle: Petrel. Model: Petrel 1. LV Configuration: Petrel P36H.
  • Particles Ionosphere mission Nation: UK. Agency: SRC. Apogee: 139 km (86 mi).

1971 -
  • Rain at the cosmodrome jeopardises Soyuz 10 launch. Nation: USSR. Program: Salyut. Flight: Soyuz 10.

1971 - Launch Vehicle: Shuttle.
  • Shuttle SSME Protest Nation: USA.

    Pratt and Whitney filed a protest against NASA's award to Rocketdyne of the SSME contract. This action prevented further work on Rocketdyne's contract until the issue was adjudicated.

1971 - Launch Site: Kwajalein. Launch Complex: Meck. Launch Pad: -. Launch Vehicle: Spartan.
  • Safeguard M1-7A Interceptor mission Nation: USA. Agency: USA. Apogee: 100 km (60 mi).

1971 - 18:59 GMT - Launch Site: Kiruna. Launch Complex: -. Launch Pad: -. Launch Vehicle: Petrel. Model: Petrel 1. LV Configuration: Petrel P64K.
  • E field Ionosphere mission Nation: UK. Agency: SRC. Apogee: 143 km (88 mi).

1971 - 21:42 GMT - Launch Site: Kiruna. Launch Complex: -. Launch Pad: -. Launch Vehicle: Petrel. Model: Petrel 1. LV Configuration: Petrel P67K.
  • Winds / E field Aurora mission Nation: UK. Agency: SRC. Apogee: 128 km (79 mi).

1971 - 23:03 GMT - Launch Site: Kiruna. Launch Complex: -. Launch Pad: -. Launch Vehicle: Petrel. Model: Petrel 1. LV Configuration: Petrel P63K.
  • E field Ionosphere mission Nation: UK. Agency: SRC. Apogee: 165 km (102 mi).

1972 - Launch Vehicle: Shuttle.
  • Shuttle SSME Contract Nation: USA.

    Rocketdyne finally receives the contact for development of the shuttle main engine. By the end of the century the total value will have exceeded $5.6 billion.

1972 - 11:59 GMT - Launch Site: Plesetsk. Launch Complex: LC133/1. Launch Pad: -. Launch Vehicle: Kosmos 2. Model: Kosmos 11K63.
  • Cosmos 487 Nation: USSR. Program: DS. Payload: DS-P1-Yu s/n 57. Mass: 325 kg (716 lb). Class: Military. Type: Target. Spacecraft: DS-P1-Yu. Agency: MO SSSR. Perigee: 269 km (167 mi). Apogee: 504 km (313 mi). Inclination: 70.00 deg. Period: 92.20 min. COSPAR: 1972-033A. USAF Sat Cat: 6006. Completed Operations Date: 1972-09-24. Decay Date: 1972-09-24.

    Development of systems for air defence and the control of outer space.

1972 - 15:13 GMT - Launch Site: White Sands. Launch Complex: LC35. Launch Pad: -. Launch Vehicle: Aerobee. Model: Aerobee 150. LV Configuration: Aerobee 150 NASA 04.208UA.
  • Aeronomy mission Nation: USA. Agency: NASA. Apogee: 200 km (120 mi).

1972 - 16:47 GMT -
  • EVA Apollo 16-1 Nation: USA. Program: Apollo. Class: Manned. Type: Lunar lander. Spacecraft: Apollo LM. Crew: Young, Duke. Flight: Apollo 16. EVA Duration: 0.30 days.

    Explored lunar surface near LM and deployed ALSEP unmanned scientific station equipment.

1975 - 08:11 GMT - Launch Site: Thumba. Launch Complex: -. Launch Pad: -. Launch Vehicle: Belier. Model: Centaure. LV Configuration: Centaure ISRO 5.26.
  • ISRO 5.26 CO.22 Ionosphere mission Nation: India. Agency: ISRO. Apogee: 157 km (97 mi).

1975 - 09:07 GMT - Launch Site: Fort Churchill. Launch Complex: -. Launch Pad: -. Launch Vehicle: Tomahawk Sandia. Model: Paiute Tomahawk. LV Configuration: Paiute Tomahawk CRL A10.302-1.
  • AEOLUS Release Aeronomy mission Nation: USA. Agency: USAF CRL. Apogee: 213 km (132 mi).

1975 - 09:07 GMT - Launch Site: Fort Churchill. Launch Complex: -. Launch Pad: -. Launch Vehicle: Tomahawk Sandia. Model: Paiute Tomahawk. LV Configuration: Paiute Tomahawk CRL A10.302-2.
  • AEOLUS Release Aeronomy mission Nation: USA. Agency: USAF CRL. Apogee: 220 km (130 mi).

1975 - 09:12 GMT - Launch Site: Fort Churchill. Launch Complex: -. Launch Pad: -. Launch Vehicle: Tomahawk Sandia. Model: Paiute Tomahawk. LV Configuration: Paiute Tomahawk CRL A10.403-1.
  • AEOLUS Mass Spectrometer Aeronomy mission Nation: USA. Agency: USAF CRL. Apogee: 222 km (137 mi).

1975 - 17:30 GMT - Launch Site: Thumba. Launch Complex: -. Launch Pad: -. Launch Vehicle: Belier. Model: Centaure. LV Configuration: Centaure ISRO 5.27.
  • ISRO 5.27 CO.21 Ionosphere mission Nation: India. Agency: ISRO. Apogee: 156 km (96 mi).

1976 - 10:00 GMT - Launch Site: White Sands. Launch Complex: -. Launch Pad: -. Launch Vehicle: Aerobee. Model: Aerobee 200A. LV Configuration: Aerobee 200A NASA 26.49DH.
  • NRL XR X-ray astronomy mission Nation: USA. Agency: NASA. Apogee: 202 km (125 mi).

1977 - 17:00 GMT - Launch Site: White Sands. Launch Complex: -. Launch Pad: -. Launch Vehicle: Aerobee. Model: Aerobee 170. LV Configuration: Aerobee 170 GL A04.410-02.
  • Solar ultraviolet / solar extreme ultraviolet mission Nation: USA. Agency: USAF GL. Apogee: 237 km (147 mi).

1978 -
  • First static firing, MPTA-098 Nation: USA. Program: STS.

    First static firing, MPTA-098, NSTL (2.5 seconds; stub nozzles)

1978 - Launch Vehicle: Shuttle.
  • Shuttle MPTA First test Nation: USA.

    For the first time three SSME engines are run on the MPTA test article mated to an external tank - for 2.5 seconds.

1978 - 05:29 GMT - Launch Site: Atlantic Ocean. Launch Complex: -. Launch Pad: 38.0 N x 75.0 W. Launch Vehicle: MR-12.
  • Aeronomy/Plasma/Solar mission Nation: USSR. Apogee: 170 km (100 mi).

1978 - 06:26 GMT - Launch Site: Atlantic Ocean. Launch Complex: -. Launch Pad: 38.0 N x 75.0 W. Launch Vehicle: MR-12.
  • Aeronomy/Plasma/Solar mission Nation: USSR. Apogee: 170 km (100 mi).

1978 - 07:52 GMT - Launch Site: Atlantic Ocean. Launch Complex: -. Launch Pad: 38.0 N x 75.0 W. Launch Vehicle: MR-12.
  • Aeronomy/Plasma/Solar mission Nation: USSR. Apogee: 150 km (90 mi).

1978 - 17:40 GMT - Launch Site: Atlantic Ocean. Launch Complex: -. Launch Pad: 38.0 N x 75.0 W. Launch Vehicle: MR-12.
  • Aeronomy/Plasma/Solar mission Nation: USSR. Apogee: 170 km (100 mi).

1978 - 18:30 GMT - Launch Site: Atlantic Ocean. Launch Complex: -. Launch Pad: 38.0 N x 75.0 W. Launch Vehicle: MR-12.
  • Aeronomy/Plasma/Solar mission Nation: USSR. Apogee: 170 km (100 mi).

1979 - 10:10 GMT - Launch Site: White Sands. Launch Complex: -. Launch Pad: -. Launch Vehicle: Black Brant. Model: Black Brant 8C. LV Configuration: Black Brant 8C NASA 27.38UE.
  • Plasma mission Nation: USA. Agency: NASA. Apogee: 317 km (196 mi).

1980 - 21:47 GMT - Launch Site: ETR Launch Area. Launch Complex: -. Launch Pad: -. Launch Vehicle: Poseidon.
  • FOT-40? Follow-on operational missile test Nation: USA. Agency: USN. Apogee: 500 km (310 mi).

1980 - 21:47 GMT - Launch Site: ETR Launch Area. Launch Complex: -. Launch Pad: -. Launch Vehicle: Poseidon.
  • FOT-40? Follow-on operational missile test Nation: USA. Agency: USN. Apogee: 500 km (310 mi).

1980 - 21:47 GMT - Launch Site: ETR Launch Area. Launch Complex: -. Launch Pad: -. Launch Vehicle: Poseidon.
  • FOT-40? Follow-on operational missile test Nation: USA. Agency: USN. Apogee: 500 km (310 mi).

1980 - 21:48 GMT - Launch Site: ETR Launch Area. Launch Complex: -. Launch Pad: -. Launch Vehicle: Poseidon.
  • FOT-40? Follow-on operational missile test Nation: USA. Agency: USN. Apogee: 500 km (310 mi).

1981 - 03:45 GMT - Launch Site: Baikonur. Launch Complex: LC90/19. Launch Pad: LC90/pad?. Launch Vehicle: Tsiklon. Model: Tsiklon-2.
  • Cosmos 1266 Nation: USSR. Program: RORSAT. Mass: 3,800 kg (8,300 lb). Class: Surveillance. Type: Naval Radarsat. Spacecraft: US-A. Agency: MO SSSR. Perigee: 911 km (566 mi). Apogee: 941 km (584 mi). Inclination: 64.80 deg. Period: 103.60 min. COSPAR: 1981-037B. USAF Sat Cat: 12429. Decay Date: 1981-05-20.

    Ocean surveillance; nuclear powered.

1982 - 01:40 GMT - Launch Site: Kapustin Yar. Launch Complex: LC107/1. Launch Pad: -. Launch Vehicle: Kosmos 3. Model: Kosmos 11K65M. LV Configuration: Kosmos 11K65M 53767-256.
  • Cosmos 1351 Nation: USSR. Mass: 550 kg (1,210 lb). Class: Calibration. Spacecraft: Taifun-2. Agency: MO SSSR. Perigee: 348 km (216 mi). Apogee: 548 km (340 mi). Inclination: 50.70 deg. Period: 93.60 min. COSPAR: 1982-034A. USAF Sat Cat: 13142. Decay Date: 1983-03-14.

    Released 25 Romb radar calibration subsatellites.

1982 - 09:15 GMT - Launch Site: Baikonur. Launch Complex: LC1. Launch Pad: LC1 or LC31. Launch Vehicle: Soyuz. Model: Soyuz 11A511U.
  • Cosmos 1352 Nation: USSR. Mass: 6,300 kg (13,800 lb). Class: Surveillance. Type: Military. Spacecraft: Zenit-6U. Agency: MOM. Perigee: 204 km (126 mi). Apogee: 364 km (226 mi). Inclination: 70.40 deg. Period: 90.10 min. COSPAR: 1982-035A. USAF Sat Cat: 13144. Duration: 14.00 days. Decay Date: 1982-05-05.

    Photo surveillance; returned film capsule.

1987 - 15:14 GMT - Launch Site: Baikonur. Launch Complex: LC1. Launch Pad: -. Launch Vehicle: Soyuz. Model: Soyuz 11A511U2.
  • Progress 29 Nation: USSR. Program: Mir. Payload: Progress s/n 127. Mass: 7,100 kg (15,600 lb). Class: Manned. Type: Logistics. Spacecraft: Progress. Agency: MOM. Perigee: 189 km (117 mi). Apogee: 237 km (147 mi). Inclination: 51.60 deg. Period: 88.80 min. COSPAR: 1987-034A. USAF Sat Cat: 17878. Duration: 19.72 days. Completed Operations Date: 1987-05-11 08:27:43 PM. Decay Date: 1987-05-11 08:27:43 PM. Flight: Mir EO-2, Mir LD-1.

    Unmanned supply vessel to Mir. Deorbited May 11, 1987. Docked with Mir at 343 X 363 1705 23 April at rear port of Kvant. Undocked May 11 03:10. Deorbited28 May 02:59 .
    Officially: Transporting sundry cargoes to the Mir orbital station. Docked with Salyut 7 on 23 Apr 1987 17:04:51 GMT. Undocked on 11 May 1987 03:10:01 GMT. Destroyed in reentry on 11 May 1987 08:28:00 GMT. Total free-flight time 2.30 days. Total docked time 17.42 days.

1990 - 10:15 GMT - Launch Site: White Sands. Launch Complex: LC36. Launch Pad: -. Launch Vehicle: Black Brant. Model: Black Brant 9. LV Configuration: Black Brant IX NASA 36.73UG.
  • JHU FOT 9 (C / Austin) Ultraviolet astronomy mission Nation: USA. Agency: NASA. Apogee: 300 km (180 mi).

1993 - 00:23 GMT - Launch Site: Plesetsk. Launch Complex: LC43/4. Launch Pad: -. Launch Vehicle: Soyuz. Model: Molniya 8K78M. LV Configuration: Molniya 8K78M-ML.
  • Molniya 3-44 Nation: Russia. Program: Molniya. Payload: Molniya-3 s/n 57. Mass: 1,600 kg (3,500 lb). Class: Communications. Spacecraft: Molniya-3. Agency: MOM. Perigee: 744 km (462 mi). Apogee: 39,603 km (24,608 mi). Inclination: 62.90 deg. Period: 717.70 min. COSPAR: 1993-025A. USAF Sat Cat: 22633. Decay Date: 2004-01-25.

    Operation of the long-range telephone and telegraph radio communications system, transmission of television programmes to stations in the Orbita network and international cooperation. Replaced Molniya 3-41.

1995 - 01:44 GMT - Launch Site: Kourou. Launch Complex: ELA2. Launch Pad: -. Launch Vehicle: Ariane. Model: Ariane 40. LV Configuration: Ariane 40+ V72.
  • ERS 2 Nation: Europe. Mass: 2,516 kg (5,546 lb). Class: Earth. Type: Radarsat. Spacecraft: ERS 1-2. Agency: ESA. Perigee: 784 km (487 mi). Apogee: 785 km (487 mi). Inclination: 98.60 deg. Period: 100.50 min. COSPAR: 1995-021A. USAF Sat Cat: 23560.

    European Remote Sensing; carried SAR; ocean, land, ice, and atmospheric observations.

1995 - 15:04 GMT - Launch Site: White Sands. Launch Complex: -. Launch Pad: -. Launch Vehicle: THAAD. LV Configuration: THAAD FT-01.
  • Test mission Nation: USA. Agency: USA. Apogee: 100 km (60 mi).

1996 - Launch Site: ETR Launch Area. Launch Complex: -. Launch Pad: -. Launch Vehicle: Trident. Model: Trident D-5. LV Configuration: Trident D-5 FCET-14.
  • Operational test Nation: USA. Agency: USN. Apogee: 1,000 km (600 mi).

1996 - Launch Site: ETR Launch Area. Launch Complex: -. Launch Pad: -. Launch Vehicle: Trident. Model: Trident D-5. LV Configuration: Trident D-5 FCET-14.
  • Nation: USA. Agency: USN. Apogee: 1,000 km (600 mi).

1997 - 11:59 GMT - Launch Site: Gran Canaria DZ. Launch Complex: -. Launch Pad: 27.0 N x 15.3 W. Launch Vehicle: Pegasus. Model: Pegasus XL. LV Configuration: Pegasus XL F15.
  • Minisat-01 Nation: USA. Mass: 209 kg (460 lb). Class: Technology . Spacecraft: Minisat. Manufacturer: CASA, Madrid. Agency: INTA. Perigee: 561 km (348 mi). Apogee: 580 km (360 mi). Inclination: 151.00 deg. Period: 96.00 min. COSPAR: 1997-018A. USAF Sat Cat: 24779. Decay Date: 2002-02-26.

    Minisat-01 carried the EURD extreme ultraviolet spectrograph to study interstellar gas, the LEGRI gamma ray burst detector, and the CPLM microacceleration in liquids experiment.

  • Celestis Nation: USA. Payload: CPAC. Class: Burial . Spacecraft: CPAC. Manufacturer: Orbital Sciences Corp., Germantown (formerly Fairchild). Agency: OSC. Perigee: 553 km (343 mi). Apogee: 581 km (361 mi). Inclination: 151.00 deg. Period: 96.00 min. COSPAR: 1997-018B. USAF Sat Cat: 24780.

1998 -
  • Chinese Manned Spacecraft Launch Set for 1999 Nation: China. Spacecraft: Shenzhou.

    Preparations for the first test launch of China's first manned spacecraft were underway at the launch site, a Shanghai newspaper reported. It said the first flight would be launched in late 1999. The space cabin, telemetry system and power system had been developed in Shanghai.

1998 -
  • China Completed New Wind Tunnels For Space Development Nation: China.

    Two special wind tunnels in southwest China's Sichuan Province were nearing completion. The new tunnels would be used for testing China's future space shuttle, launch vehicles, and strategic missiles. A high-frequency plasma wind tunnel and a supersonic flow wind tunnel were being built by China Aerodynamics Research and Development Center and would be the most advanced in Asia.

1999 - 04:59 GMT - Launch Site: Baikonur. Launch Complex: LC109. Launch Pad: LC109/95. Launch Vehicle: R-36M. Model: Dnepr. LV Configuration: Dnepr 6703542509.
  • UoSAT-12 Nation: UK. Mass: 325 kg (716 lb). Class: Technology. Spacecraft: MiniSat-400. Manufacturer: Surrey. Agency: SSTL. Perigee: 639 km (397 mi). Apogee: 654 km (406 mi). Inclination: 64.60 deg. Period: 97.70 min. COSPAR: 1999-021A. USAF Sat Cat: 25693.

    First launch of Russia's Dnepr launch vehicle, a converted R-36M2 ICBM. The Dnepr was launched from a silo. The third stage maneuvring bus (used on the ICBM for dispensing multiple warheads) placed UoSAT-12 into a 638 km x 652 km x 64.6 deg orbit. The third stage separated from the payload at 05:13 GMT and then made a burn into a 599 km x 1403 km x 64.6 deg orbit. UoSAT-12 was the first test of the Minibus platform, at 325 kg a larger spacecraft than earlier 50 kg Surrey UoSATs. It carried a mobile radio experiment (MERLION), a GPS receiver, and imaging cameras.

2007 - 12:31 GMT -
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