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1933 - Launch Vehicle: GIRD-09. FAILURE: Failure.

  • GIRD-09 launch attempt. Nation: USSR.

    Launch failure.

1950 - Launch Vehicle: G-4.
  • German assistance to Soviet rocketry to be ended. Nation: USSR.

    Decree 3456-1446 'On termination or the work of German scientists in the Soviet missile program.' was issued.

1953 - Launch Site: White Sands. Launch Complex: LC33. Launch Pad: -. Launch Vehicle: Hermes. Model: Hermes A-3A. LV Configuration: Hermes A-3A 3.
  • Test mission Nation: USA. Agency: USA. Apogee: 30 km (18 mi).

1954 - Launch Vehicle: Kosmos 2. Model: R-12.
  • R-12 development authorised. Nation: USSR.

    Decree 'On the Creation and preparation of the R-12 (8K63) missile--start of work an the R-12' was issued.

1957 - Launch Site: Kapustin Yar. Launch Complex: V-2. Launch Pad: -. Launch Vehicle: R-2. Model: R-2A.
  • SOI Solar ultraviolet mission Nation: USSR. Agency: NII-88. Apogee: 100 km (60 mi).

1957 - 01:58 GMT - Launch Site: Atlantic Ocean. Launch Complex: -. Launch Pad: 60.6 N x 49.3 W. Launch Vehicle: Rockoon. Model: Loki Rockoon. LV Configuration: Loki Rockoon II5.14F.
  • SUI 69 Aeronomy / aurora / chemical release mission Nation: USA. Agency: SUI. Apogee: 100 km (60 mi).

    Launched at IGY Rockoon Launch Site 1, Atlantic Ocean LP14 - - Latitude: 60.58 N - Longitude: 49.27 W.

1958 - Launch Site: Kapustin Yar. Launch Complex: -. Launch Pad: -. Launch Vehicle: R-2. Model: R-2A.
  • R-2A launch Nation: USSR. Agency: NII-88. Apogee: 212 km (131 mi).

1958 - Launch Site: Holloman. Launch Complex: A. Launch Pad: -. Launch Vehicle: Aerobee. Model: Aerobee.
  • Ionosphere mission Nation: USA. Agency: USAF. Apogee: 100 km (60 mi).

1958 - 02:00 GMT - Launch Site: Kapustin Yar. Launch Complex: V-2. Launch Pad: -. Launch Vehicle: R-2. Model: R-2A. LV Configuration: R-2A No. 7.
  • Ionosphere / biological mission Nation: USSR. Agency: AN SSSR. Apogee: 212 km (131 mi).

1959 - 19:00 GMT - Launch Site: Vandenberg. Launch Complex: SLC1W. Launch Pad: -. Launch Vehicle: Delta. Model: Thor Agena A. LV Configuration: Thor Agena A 192 / Agena A 1029.
  • Discoverer 5 Nation: USA. Payload: KH-1 9002 / Agena A 1029. Mass: 781 kg (1,721 lb). Class: Surveillance. Type: Military. Spacecraft: KH-1. Agency: DARPA. Perigee: 214 km (132 mi). Apogee: 731 km (454 mi). Inclination: 79.90 deg. Period: 94.10 min. COSPAR: 1959-Epsilon-1. USAF Sat Cat: 18. Decay Date: 1959-09-28.

    KH-1; 1st generation low resolution photo surveillance; film capsule boosted into higher orbit, decayed 2/11/61. Mission failed. Power supply failure. No recovery.

  • Discoverer 5 Capsule Nation: USA. Payload: KH-1 9002 Capsule. Class: Surveillance. Type: Military. Spacecraft: KH-1. Agency: USAF. Perigee: 218 km (135 mi). Apogee: 1,700 km (1,000 mi). Inclination: 78.90 deg. Period: 104.30 min. COSPAR: 1959-Epsilon-2. USAF Sat Cat: 26. Decay Date: 1961-02-11.

    KH-1; 1st generation low resolution photo surveillance; film capsule boosted into higher orbit, decayed 2/11/61. Mission failed. Power supply failure. No recovery.

1959 - 23:14 GMT - Launch Site: Baikonur. Launch Complex: LC1. Launch Pad: -. Launch Vehicle: Soyuz. Model: R-7.
  • GCh No. IZ-25 (III) test Nation: USSR. Agency: MVS. Apogee: 1,350 km (830 mi).

1960 -
  • Army mapping of lunar landing sites completed. Nation: USA. Program: Apollo.

    Army announced completion of a project for mapping lunar landing sites.

1960 -
  • First photo-geological survey of the surface of the moon Nation: USA. Program: Apollo.

    Secretary of the Interior Fred A. Seaton and Secretary of the Army Wilber M. Brucker announced that the U.S. Geological Survey had completed the first known photogeological survey of the surface of the moon. - Additional details.

1960 - 07:19 GMT - Launch Site: Eglin. Launch Complex: -. Launch Pad: -. Launch Vehicle: Viper. Model: Viper Falcon.
  • TP Annie Aeronomy mission Nation: USA. Agency: USAF. Apogee: 120 km (70 mi).

1960 - 09:47 GMT - Launch Site: Eglin. Launch Complex: -. Launch Pad: -. Launch Vehicle: Viper. Model: Viper Falcon.
  • TP Norma Aeronomy mission Nation: USA. Agency: USAF. Apogee: 97 km (60 mi).

1961 -
  • East Germans erect Berlin Wall between East and West Berlin to halt flood of refugees Nation: Germany.

1961 - Launch Site: Baikonur. Launch Complex: LC41/4. Launch Pad: -. Launch Vehicle: R-16. LV Configuration: R-16 21L. FAILURE: Failure.
  • Test mission Nation: USSR. Agency: RVSN. Apogee: 0 km ( mi).

1962 -
  • Ten Air Force pilots spend a month in a simulated space cabin Nation: USA. Program: Apollo.

    Ten Air Force pilots emerged from a simulated space cabin in which they had spent the previous month participating in a psychological test to determine how long a team of astronauts could work efficiently on a prolonged mission in space. Project Director Earl Alluisi said the experiment had "far exceeded our expectations" and that the men could have stayed in the cabin for 40 days with no difficulty.

1962 - 22:00 GMT - Launch Site: Cape Canaveral. Launch Complex: LC11. Launch Pad: -. Launch Vehicle: Atlas. Model: Atlas F. LV Configuration: Atlas F 7F.
  • Research and development / Pod 16 test Nation: USA. Agency: USAF. Apogee: 1,400 km (800 mi).

1963 - Launch Site: Cape Canaveral. Launch Complex: LC25A. Launch Pad: -. Launch Vehicle: Polaris. Model: Polaris A3. LV Configuration: Polaris A3X-36.
  • Test mission Nation: USA. Agency: USN. Apogee: 1,000 km (600 mi).

1963 - 04:59 GMT - Launch Site: Baikonur. Launch Complex: LC41/15. Launch Pad: -. Launch Vehicle: R-16. Model: R-16U.
  • Combat training launch Nation: USSR. Agency: RVSN. Apogee: 757 km (470 mi).

1964 - Launch Site: Vandenberg. Launch Complex: 395-B. Launch Pad: -. Launch Vehicle: Titan. Model: Titan 2. LV Configuration: Titan II B-7.
  • Gentle Annie Nation: USA. Agency: USAF SAC. Apogee: 1,300 km (800 mi).

    Demonstration and shakedown operations launch

1965 - Launch Site: Vandenberg. Launch Complex: -. Launch Pad: -.
  • Last launch of Thor/Able-Star from Vandenberg AFB. Nation: USA.

    Last launch of Thor/Able-Star from Vandenberg AFB. (first launch on 28 September 1963).

1965 - Launch Site: Baikonur. Launch Complex: PU33. Launch Pad: -. Launch Vehicle: Tsiklon. Model: R-36 8K67.
  • State trials missile test Nation: USSR. Agency: RVSN. Apogee: 1,000 km (600 mi).

1965 - 22:11 GMT - Launch Site: Vandenberg. Launch Complex: SLC2E. Launch Pad: -. Launch Vehicle: Delta. Model: Thor Ablestar. LV Configuration: Thor Ablestar-2 455 AB020.
  • Dodecapole 2 Nation: USA. Payload: PORCUPINE 2. Mass: 4.00 kg (8.80 lb). Class: Calibration. Spacecraft: DODECAPOLE. Agency: USN. Perigee: 979 km (608 mi). Apogee: 1,051 km (653 mi). Inclination: 90.00 deg. Period: 105.40 min. COSPAR: 1965-065C. USAF Sat Cat: 1510.

    Surveillance Calibration; dodecahedron; extended 12 25 ft. antennas. Space craft engaged in investigation of spaceflight techniques and technology (US Cat A).

  • Tempsat 1 Nation: USA. Mass: 9.00 kg (19.80 lb). Class: Calibration. Spacecraft: Tempsat. Agency: USN. Perigee: 1,082 km (672 mi). Apogee: 1,188 km (738 mi). Inclination: 89.90 deg. Period: 108.00 min. COSPAR: 1965-065E. USAF Sat Cat: 1512.

    Surveillance Calibration; black 14 inch dia. sphere. Space craft engaged in investigation of spaceflight techniques and technology (US Cat A).

  • Transit O-5 Nation: USA. Program: Transit. Payload: NNS 30050. Mass: 61 kg (134 lb). Class: Navigation. Spacecraft: Transit. Agency: USN. Perigee: 1,078 km (669 mi). Apogee: 1,183 km (735 mi). Inclination: 89.90 deg. Period: 107.90 min. COSPAR: 1965-065F. USAF Sat Cat: 1514.

    Naval Avionics Facility-assembled production spacecraft. Failed after a few weeks operation.

  • Long Rod Nation: USA. Payload: Navspasur Rod. Class: Calibration. Spacecraft: Surcal. Agency: USN. Perigee: 1,090 km (670 mi). Apogee: 1,194 km (741 mi). Inclination: 90.00 deg. Period: 108.10 min. COSPAR: 1965-065G. USAF Sat Cat: 1515.

    Space craft engaged in investigation of spaceflight techniques and technology (US Cat A).

  • Calsphere 4A Nation: USA. Payload: NRL PL 158?. Mass: 2.00 kg (4.40 lb). Class: Calibration. Spacecraft: Calsphere. Agency: USN. Perigee: 1,077 km (669 mi). Apogee: 1,179 km (732 mi). Inclination: 90.10 deg. Period: 107.90 min. COSPAR: 1965-065H. USAF Sat Cat: 1520.

    Surveillance Calibration; white 14 inch dia. sphere.

  • SURCAL 5 Nation: USA. Payload: NRL PL150C?. Class: Calibration. Spacecraft: SURCAL. Agency: USN. Perigee: 1,083 km (672 mi). Apogee: 1,196 km (743 mi). Inclination: 90.00 deg. Period: 108.11 min. COSPAR: 1965-065K. USAF Sat Cat: 1521.

1968 - Launch Vehicle: Saturn V.
  • Borman crew selected for Apollo 8 lunar mission. Nation: USA. Program: Apollo. Spacecraft: Apollo CSM. Flight: Apollo 8, Apollo 9.

    Kleinknecht had concluded his CSM 103-106 configuration study by August 13 and determined the high-gain antenna was the most critical item. Kraft was still "GO" and said December 20-26 (except December 25) offered best launch times; he had also looked at January launch possibilities. Slayton had decided to assign the 104 crew to the mission. He had talked to crew commander Frank Borman and Borman was interested.

1969 - Launch Site: Kwajalein. Launch Complex: Meck. Launch Pad: -. Launch Vehicle: Spartan. LV Configuration: Spartan ABM 800012. FAILURE: Failure.
  • KT-12 test Nation: USA. Agency: USA. Apogee: 0 km ( mi).

1969 - 04:23 GMT - Launch Site: Fort Churchill. Launch Complex: -. Launch Pad: -. Launch Vehicle: Nike. Model: Nike Iroquois. LV Configuration: Nike Iroquois CRL A07.902-2.
  • Mass spectrometer Aeronomy mission Nation: USA. Agency: USAF. Apogee: 114 km (70 mi).

1969 - 06:30 GMT - Launch Site: White Sands. Launch Complex: -. Launch Pad: -. Launch Vehicle: Apache. Model: Nike Apache. LV Configuration: Nike Apache NASA 14.422UA.
  • Pandora K (Perseids) Aeronomy / meteorites mission Nation: USA. Agency: NASA. Apogee: 143 km (88 mi).

1969 - 22:00 GMT - Launch Site: Plesetsk. Launch Complex: LC132/1. Launch Pad: LC132/pad?. Launch Vehicle: Kosmos 3. Model: Kosmos 11K65M.
  • Cosmos 292 Nation: USSR. Mass: 775 kg (1,708 lb). Class: Navigation. Spacecraft: Tsiklon. Agency: MO SSSR. Perigee: 719 km (446 mi). Apogee: 733 km (455 mi). Inclination: 74.10 deg. Period: 99.30 min. COSPAR: 1969-070A. USAF Sat Cat: 4070.

    Military navigation satellite.

1970 - 16:31 GMT - Launch Site: Wallops Island. Launch Complex: -. Launch Pad: -. Launch Vehicle: Aerobee. Model: Aerobee 350. LV Configuration: Aerobee 350 NASA 17.06UE.
  • ECHO I Plasma mission Nation: USA. Agency: NASA. Apogee: 350 km (210 mi).

1970 - 19:02 GMT - Launch Site: White Sands. Launch Complex: LC35. Launch Pad: -. Launch Vehicle: Aerobee. Model: Aerobee 150. LV Configuration: Aerobee 150 NASA 04.200DS.
  • NRL NE3.247 Solar mission Nation: USA. Agency: NASA. Apogee: 200 km (120 mi).

1971 - Launch Site: Vandenberg. Launch Complex: LF05. Launch Pad: -. Launch Vehicle: Minuteman 2.
  • OT GT87M operational test launch Nation: USA. Agency: USAF SAC. Apogee: 1,300 km (800 mi).

1971 - 16:00 GMT - Launch Site: Green River. Launch Complex: -. Launch Pad: -. Launch Vehicle: Athena RTV. Model: Athena H. LV Configuration: Athena H H002.
  • ADE-2 re-entry vehicle test flight Nation: USA. Agency: USAF. Apogee: 200 km (120 mi).

1972 - 06:59 GMT - Launch Site: Thumba. Launch Complex: -. Launch Pad: -. Launch Vehicle: Apache. Model: Nike Apache. LV Configuration: Nike Apache ISRO 10.44.
  • ISRO 10.44 Ionosphere mission Nation: India. Agency: ISRO. Apogee: 148 km (91 mi).

1972 - 15:10 GMT - Launch Site: Wallops Island. Launch Complex: LA3A. Launch Pad: -. Launch Vehicle: Scout. Model: Scout D-1. LV Configuration: Scout D-1-F S184C.
  • Explorer 46 Nation: USA. Program: Explorer. Payload: Meteoroid Technology Satellite. Mass: 136 kg (299 lb). Class: Earth. Type: Micrometeoroid. Spacecraft: MTS. Agency: NASA LaR. Perigee: 492 km (305 mi). Apogee: 811 km (503 mi). Inclination: 37.70 deg. Period: 97.70 min. COSPAR: 1972-061A. USAF Sat Cat: 6142. Decay Date: 1979-11-02.

    Micrometeoroid tests. Spacecraft engaged in research and exploration of the upper atmosphere or outer space (US Cat B).

1973 -
  • Skylab backup Saturn V Orbital Workshop launch capability cancelled. Nation: USA. Program: Skylab. Spacecraft: Skylab.

    NASA decided to delete the Skylab backup Saturn V Orbital Workshop launch capability effective 15 August. All work associated with the completion, checkout, and support of Skylab backup hardware, experiments, software, facilities, and ground support equipment would be canceled immediately, except for the work that would directly support SL-3, SL-4, and rescue missions.

1974 - Launch Vehicle: RLA.
  • Glushko briefed his new RLA launch vehicle family to the VPK Military Industrial Commission Nation: USSR.

    These RLA - Rocket Flight Apparatus - met the requirements of the Ministry of Defence as described in 1973 in Plan Poisk and would replace the failed N1 and all existing launch vehicles. As required by the Ministry of Defence, they used only Lox/Kerosene propellants; the various launch vehicles were modular, and used common engines and rocket bodies. The members of the VPK met the proposal with considerable scepticism. The final decision was that the plan had to be reworked. - Additional details.

1974 - Launch Vehicle: Energia, N1.
  • N1 work cancelled Nation: USSR. Program: Lunar L3. Spacecraft: LK, Soyuz 7K-LOK, Buran.

    Glushko formally cancelled the N1 within the new NPO Energia on 13 August 1974 with the support of Ustinov, even though he had no decree of the VPK Military-Industrial Commission or the Central Committee authorising such an act. The N1-L3 itself was not officially closed down until the resolution of February 1976 starting work on the Energia/Buran boosters. By that time 6 billion roubles had been spent on the N1 over 17 years. - Additional details.

1975 - 07:21 GMT - Launch Site: Baikonur. Launch Complex: LC1. Launch Pad: LC1 or LC31. Launch Vehicle: Soyuz. Model: Voskhod 11A57.
  • Cosmos 754 Nation: USSR. Mass: 6,300 kg (13,800 lb). Class: Surveillance. Type: Military. Spacecraft: Zenit-4MK. Agency: MOM. Perigee: 204 km (126 mi). Apogee: 326 km (202 mi). Inclination: 71.40 deg. Period: 89.80 min. COSPAR: 1975-073A. USAF Sat Cat: 8069. Duration: 13.00 days. Decay Date: 1975-08-26.

    High resolution photo reconnaissance satellite; returned film capsule; maneuverable.

1978 - 00:58 GMT - Launch Site: Kiruna. Launch Complex: -. Launch Pad: -. Launch Vehicle: Petrel. Model: Petrel 1. LV Configuration: Petrel P206K.
  • Atomic oxygen Aeronomy mission Nation: UK. Agency: SRC. Apogee: 150 km (90 mi).

1979 -
  • Ferry flight, Tulsa to Denver Nation: USA. Program: STS. Class: Manned. Type: Spaceplane. Spacecraft: Enterprise.

    Ferry flight, shuttle carrier aircraft/Enterprise (OV-101), Tulsa to Denver (2 hours)

1981 - 02:26 GMT - Launch Site: ETR Launch Area. Launch Complex: -. Launch Pad: -. Launch Vehicle: Trident. Model: Trident C-4.
  • OT-6 Operational missile test Nation: USA. Agency: USN. Apogee: 1,000 km (600 mi).

1981 - 02:46 GMT - Launch Site: ETR Launch Area. Launch Complex: -. Launch Pad: -. Launch Vehicle: Trident. Model: Trident C-4.
  • OT-6 Operational missile test Nation: USA. Agency: USN. Apogee: 1,000 km (600 mi).

1981 - 03:32 GMT - Launch Site: ETR Launch Area. Launch Complex: -. Launch Pad: -. Launch Vehicle: Trident. Model: Trident C-4.
  • OT-6 Operational missile test Nation: USA. Agency: USN. Apogee: 1,000 km (600 mi).

1981 - 03:32 GMT - Launch Site: ETR Launch Area. Launch Complex: -. Launch Pad: -. Launch Vehicle: Trident. Model: Trident C-4.
  • OT-6 Operational missile test Nation: USA. Agency: USN. Apogee: 1,000 km (600 mi).

1981 - 16:20 GMT - Launch Site: Plesetsk. Launch Complex: LC41/1. Launch Pad: -. Launch Vehicle: Soyuz. Model: Soyuz 11A511U.
  • Cosmos 1296 Nation: USSR. Payload: Yantar-2K s/n 943. Mass: 6,600 kg (14,500 lb). Class: Surveillance. Type: Military. Spacecraft: Yantar-2K. Agency: MOM. Perigee: 167 km (103 mi). Apogee: 354 km (219 mi). Inclination: 67.10 deg. Period: 89.70 min. COSPAR: 1981-078A. USAF Sat Cat: 12687. Duration: 31.00 days. Decay Date: 1981-09-13.

    Area survey photo reconnaissance; returned film in two small SpK capsules during the mission and with the main capsule at completion of the mission.

1989 - 09:00 GMT - Launch Site: Poker Flat. Launch Complex: -. Launch Pad: -. Launch Vehicle: Black Brant. Model: Black Brant 8C. LV Configuration: Black Brant 8C SP-4 DRO-0402.
  • CHEER / Black Star 2 Target mission Nation: USA. Agency: SDIO. Apogee: 340 km (210 mi).

1989 -
  • Landing of STS-28 Nation: USA. Program: STS. Flight: STS-28.

    STS-28 landed at 13:43 GMT.

1992 - 23:00 GMT - Launch Site: Xichang. Launch Complex: LC2. Launch Pad: -. Launch Vehicle: CZ. Model: CZ-2E. LV Configuration: Chang Zheng 2E CZ2E-2 (28).
  • Optus B1 Nation: Australia. Program: Aussat. Payload: Aussat B1. Mass: 2,760 kg (6,080 lb). Class: Communications. Spacecraft: HS 601. Agency: Optus. Perigee: 35,774 km (22,228 mi). Apogee: 35,800 km (22,200 mi). Inclination: 0.00 deg. Period: 1,436.10 min. COSPAR: 1992-054A. USAF Sat Cat: 22087.

    Stationed at 160 deg E. Commercial communications. Longitude 160 +/- 0.05 deg E. Launched fromn China. Positioned in geosynchronous orbit at 160 deg E in 1992-1999 As of 1 September 2001 located at 159.98 deg E drifting at 0.009 deg W per day. As of 2007 Mar 11 located at 163.63E drifting at 0.044E degrees per day.

1997 - 13:50 GMT - Launch Site: Wallops Island. Launch Complex: -. Launch Pad: -. Launch Vehicle: Loki. Model: Super Loki. LV Configuration: Super Loki Sphere.
  • CRISTA Aeronomy mission Nation: USA. Agency: NASA. Apogee: 117 km (72 mi).

1997 - 13:55 GMT - Launch Site: Wallops Island. Launch Complex: -. Launch Pad: -. Launch Vehicle: Loki. Model: Super Loki. LV Configuration: Super Loki Sphere.
  • CRISTA Aeronomy mission Nation: USA. Agency: NASA. Apogee: 121 km (75 mi).

1997 - 21:40 GMT - Launch Site: Wallops Island. Launch Complex: -. Launch Pad: -. Launch Vehicle: Loki. Model: Super Loki. LV Configuration: Super Loki Sphere.
  • CRISTA Aeronomy mission Nation: USA. Agency: NASA. Apogee: 121 km (75 mi).

1998 - 09:43 GMT - Launch Site: Baikonur. Launch Complex: LC1. Launch Pad: -. Launch Vehicle: Soyuz. Model: Soyuz 11A511U.
  • Soyuz TM-28 Nation: Russia. Program: Mir. Payload: Soyuz TM 11F732 s/n 77. Class: Manned. Type: Spacecraft. Spacecraft: Soyuz TM. Manufacturer: RKK Energiya im. S.P. Korolyov, Kaliningrad-Korolyov. Agency: RKA. Perigee: 363 km (225 mi). Apogee: 373 km (231 mi). Inclination: 51.70 deg. Period: 91.90 min. COSPAR: 1998-047A. USAF Sat Cat: 25429. Duration: 198.69 days. Decay Date: 1999-02-28. Crew: Padalka, Avdeyev, Baturin. Flight: Mir EP-4, Mir EO-26, Mir EO-25, Mir EO-26/-27.

    Soyuz TM-28 docked at 10:56 GMT on August 15 with the rear (Kvant) port of the Mir space station, which had been vacated at 09:28 GMT on August 12 by Progress M-39. The EO-25 crew, Musabayev and Budarin, landed with Baturin on Aug 25, leaving the EO-26 crew of Padalka and Avdeyev on the station. As only one final Soyuz mission to Mir was planned, with two of the seats on that Soyuz pre-sold to Slovak and French experimenters, the return crew of Soyuz TM-28 was subject to constant replanning and revision. On February 8, 1999, at 11:23 GMT Padalka and Avdeyev undocked from Mir's -X port in Soyuz TM-28, and redocked at the +X Kvant port at 11:39 GMT, freeing up the front port for the Soyuz TM-29 docking. Finally on February 27, 1999 EO-26 commander Padalka and Slovak cosmonaut Bella undocked Soyuz TM-28 from the Kvant rear docking port at 22:52 GMT, landing in Kazakhstan on February 28 at 02:14 GMT. Avdeyev remained on Mir with the EO-27 crew delivered on Soyuz TM-29, heading for a manned space flight time record.

2003 - 02:09 GMT - Launch Site: Point Arguello WADZ. Launch Complex: -. Launch Pad: 36.0 N x 123.0 W. Launch Vehicle: Pegasus. Model: Pegasus XL. LV Configuration: Pegasus XL F35.
  • Scisat 1 Nation: Canada. Mass: 260 kg (570 lb). Class: Ozone Monitoring. Spacecraft: SCISAT. Agency: Canadian Space Agency. Perigee: 642 km (398 mi). Apogee: 654 km (406 mi). Inclination: 73.90 deg. Period: 97.70 min. COSPAR: 2003-036A. USAF Sat Cat: 27858.

    Canadian Space Agency spacecraft which carried the ACE-FTS spectrometer to study the chemistry of the upper troposphere and stratosphere and the MAESTRO instrument to study ozone and aerosol levels in the atmosphere. Originally to have launched June 25, 2002. Delayed five more times.

2005 - 23:28 GMT - Launch Site: Baikonur. Launch Complex: LC31. Launch Pad: -. Launch Vehicle: Soyuz. Model: Soyuz FG. LV Configuration: Soyuz-FG Zh15000-011 / Fregat ST-13 sn 007.
  • Galaxy 14 Nation: USA. Program: Galaxy. Mass: 2,087 kg (4,601 lb). Class: Communications. Spacecraft: Star bus. Manufacturer: Orbital Sciences. Agency: PanAmSat. Perigee: 35,782 km (22,233 mi). Apogee: 35,790 km (22,230 mi). Inclination: 0.00 deg. Period: 1,436.10 min. COSPAR: 2005-030A. USAF Sat Cat: 28790.

    Payload swapped from Ariane 5. Launch delayed from December 2004; February 25, March 16 and 25, April 25, June 17, July 10 and 28, August 1, 6 and 12, 2005. As of 2007 Mar 9 located at 125.05W drifting at 0.008W degrees per day.

2007 - 05:45 GMT - Launch Site: White Sands. Launch Complex: -. Launch Pad: -. Launch Vehicle: Black Brant. Model: Black Brant 9. LV Configuration: Black Brant IX NASA 36.220UG.
  • JHU FOT 18 / LIDOS 2 Ultraviolet astronomy mission Nation: USA. Agency: NASA GSFC. Apogee: 278 km (172 mi).


Born on this day in:
  • 1943 - Yuri Fedorovich Isaulov.  Russian Pilot Cosmonaut. Birth City: Omsk. Birth State: Omsk. Birth Country: Russia.

Died on this day in:
  • 1980 - Konstantin Nikolayevich Rudnev.  Russian Government Official.
  • 1996 - DeMarquis D Wyatt.  American Manager.

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