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On February 6 in Space History
1911 February 6 - .
- Birth of Ronald Reagan - .
Nation: USA.
Related Persons: Reagan.
American politician, president of the USA 1981-1989. Initiated 'Star Wars' strategic defences and Space Station Freedomt. Confronted the Soviet Union with a heavy aerospace buildup which they could not match, contributing to their collapse..
1919 February 6 - .
- Birth of John Harrison - .
Nation: USA.
Related Persons: Harrison.
American engineer. Manager of Test Operations for the Atlas-Centaur and Titan 3E-Centaur..
1945 February 6 - .
15:21 GMT - .
Launch Site:
V-2 Battery 836.
Launch Pad: 1./836.
Launch Vehicle:
V-2.
- V-2 combat launch from Hachenburg to Wilrijk - .
Nation: Germany.
Hachenburg, Hillscheid, rocket fired impacted Boomsesteenweg, Wilrijk. 2 Dead..
1948 February 6 - .
17:17 GMT - .
Launch Site:
White Sands.
Launch Complex:
White Sands LC33.
Launch Vehicle:
V-2.
- Test mission - .
Nation: USA.
Agency: GE.
Apogee: 113 km (70 mi). Launched 10:15 local time. Reached 111.3 km. Carried No upper atmosphere experiments. Technology flight for General Electric. Successful electronic flight control demonstrated by General Electric technicians for Army Ordnance..
1951 February 6 - .
17:20 GMT - .
Launch Site:
White Sands.
Launch Complex:
White Sands LC35.
LV Family:
Aerobee.
Launch Vehicle:
Aerobee RTV-N-10.
- Earth photography Imaging mission - .
Nation: USA.
Agency: APL.
Apogee: 98 km (60 mi). Photography research. Launched at 1020 local time. Reached 98.2 km..
1958 February 6 - .
- Committee on Space and Astronautics - .
Nation: USA.
The Senate passed a resolution (S Res 256) creating a special Committee on Space and Astronautics to frame legislation for a national program for space exploration..
1959 February 6 - .
- Formal contract for 12 Mercury spacecraft with McDonnell. - .
Nation: USA.
Spacecraft: Mercury.
Following industry-wide competition, a formal contract for research and development of the Mercury spacecraft was negotiated with the McDonnell Aircraft Corporation. The contract called for design and construction of 12 Mercury spacecraft, but it did not include details on changes and ground support equipment which were to be negotiated as the project developed. Later, orders were placed with the company for eight additional spacecraft, two procedural trainers, an environmental trainer, and seven checkout trainers. McDonnell had been engaged in studying the development of a manned spacecraft since the NACA presentation in mid-March of 1958.
1959 February 6 - .
21:22 GMT - .
Launch Site:
Cape Canaveral.
Launch Complex:
Cape Canaveral LC15.
LV Family:
Titan.
Launch Vehicle:
Titan I.
- Nation: USA.
Agency: USAF.
Apogee: 1,000 km (600 mi). First test launch of USAF Titan ICBM (A-3) from Cape Canaveral. Dummy second stage (500 km range)..
1961 February 6 - .
- Birth of Yuri Ivanovich Onufrienko - .
Nation: Ukraine.
Related Persons: Onufrienko.
Ukrainian pilot cosmonaut 1989-2004. After leaving cosmonaut corps in April 2004, assigned as Deputy Chief for the First Administration of RGNII TsPK. Call sign: Skif (Skif - Roman-age tribe). 389 cumulative days in space. 2 spaceflights, 389.6 days in space. Flew to orbit on Soyuz TM-23 (1996), STS-108.
1961 February 6 - .
21:40 GMT - .
Launch Site:
Cape Canaveral.
Launch Complex:
Cape Canaveral LC25A.
LV Family:
Polaris.
Launch Vehicle:
Polaris A2.
FAILURE: Failure.
- Test mission - .
Nation: USA.
Agency: USN.
Apogee: 0 km (0 mi).
1962 February 6 - .
- Langley presentation of lunar orbit rendezvous - .
Nation: USA.
Program: Apollo.
Spacecraft: Apollo LM,
LM Mode Debate,
LM Source Selection.
John C. Houbolt of Langley Research Center and Charles W. Mathews of MSC made a presentation of lunar orbit rendezvous versus earth orbit rendezvous to the Manned Space Flight Management Council..
1963 February 6 - .
17:59 GMT - .
Launch Site:
Cape Canaveral.
Launch Complex:
Cape Canaveral LC15.
LV Family:
Titan.
Launch Vehicle:
Titan II.
- Mk 6 re-entry vehicle test launch - .
Nation: USA.
Agency: USAF AFSC.
Apogee: 1,300 km (800 mi). A Titan II (N-16) completed a 6,500-mile flight down the Atlantic Missile Range carrying the heaviest payload ever to travel that far on a U.S. missile..
1964 February 6 - .
- Tsien and Mao - .
Nation: China.
Related Persons: Tsien.
Tsien tutors Mao on science. This is one of only six times that Tsien actually met Mao..
1964 February 6 - .
Launch Site:
Baikonur.
Launch Complex:
Baikonur LC41/3.
LV Family:
R-16.
Launch Vehicle:
R-16U.
- Operational test launch - .
Nation: Russia.
Agency: RVSN.
Apogee: 1,210 km (750 mi).
1965 February 6 - .
Launch Site:
Cape Canaveral.
Launch Complex:
Cape Canaveral ETR.
Launch Platform: SSBN 624.
LV Family:
Polaris.
Launch Vehicle:
Polaris A2.
- Operational test - .
Nation: USA.
Agency: USN.
Apogee: 1,000 km (600 mi).
1965 February 6 - .
Launch Site:
Cape Canaveral.
Launch Complex:
Cape Canaveral ETR.
Launch Platform: SSBN 624.
LV Family:
Polaris.
Launch Vehicle:
Polaris A2.
- Operational test - .
Nation: USA.
Agency: USN.
Apogee: 1,000 km (600 mi).
1965 February 6 - .
Launch Site:
Cape Canaveral.
Launch Complex:
Cape Canaveral ETR.
Launch Platform: SSBN 624.
LV Family:
Polaris.
Launch Vehicle:
Polaris A2.
- Operational test - .
Nation: USA.
Agency: USN.
Apogee: 1,000 km (600 mi).
1965 February 6 - .
Launch Site:
Cape Canaveral.
Launch Complex:
Cape Canaveral ETR.
Launch Platform: SSBN 624.
LV Family:
Polaris.
Launch Vehicle:
Polaris A2.
- Operational test - .
Nation: USA.
Agency: USN.
Apogee: 1,000 km (600 mi).
1965 February 6 - .
05:01 GMT - .
Launch Site:
Kagoshima.
LV Family:
Kappa.
Launch Vehicle:
Kappa 9M.
- Ionosphere mission - .
Nation: Japan.
Agency: ISAS.
Apogee: 325 km (201 mi).
1965 February 6 - .
10:02 GMT - .
Launch Site:
Kagoshima.
LV Family:
Kappa.
Launch Vehicle:
Kappa 9M.
- Solar radio frequencies mission - .
Nation: Japan.
Agency: ISAS.
Apogee: 335 km (208 mi).
1967 February 6 - .
02:10 GMT - .
Launch Site:
Kagoshima.
Launch Complex:
Kagoshima L.
LV Family:
Lambda.
Launch Vehicle:
Lambda 3H.
- Ionosphere / chemical release / x-ray astronomy mission - .
Nation: Japan.
Agency: ISAS.
Apogee: 2,150 km (1,330 mi).
1968 February 6 - .
- L1 commander assignments agreed. - .
Nation: Russia.
Related Persons: Bykovsky,
Feoktistov,
Leonov,
Mishin,
Popovich,
Voloshin.
Program: Lunar L1,
Soyuz.
The final medical report rejects Feoktistov's fitness to be a cosmonaut. Mishin accepts the findings of the report, but in classic manner ignores it and advocates Feoktistov be appointed as commander of the active spacecraft in the first Soyuz docking mission after return to flight. Kamanin is livid. Feoktistov has had years of training for EVA, but he has not had one day of training as a spacecraft commander, and now he wants him to command a mission due to launch in only two to three months! However agreement is finally reached on L1 commander assignments: Leonov, Bykovskiy, Popovich, Voloshin. Agreement is not reached on the second (civilian) crew member position for the flights. According to Mishin, the Soyuz and L1 flights planned from March 1 to the end of 1968 will require 16 to 18 crew members total.
1968 February 6 - .
05:07 GMT - .
Launch Site:
Fort Churchill.
LV Family:
Tomahawk.
Launch Vehicle:
Nike Tomahawk.
- UNH Aurora / Fields Plasma mission - .
Nation: USA.
Agency: NASA.
Apogee: 270 km (160 mi).
1968 February 6 - .
07:21 GMT - .
Launch Site:
Fort Churchill.
LV Family:
Tomahawk.
Launch Vehicle:
Nike Tomahawk.
- Aurora Aurora mission - .
Nation: USA.
Agency: Sandia.
Apogee: 160 km (90 mi).
1968 February 6 - .
08:00 GMT - .
Launch Site:
Baikonur.
Launch Complex:
Baikonur LC1.
Launch Pad: LC31.
LV Family:
R-7.
Launch Vehicle:
Voskhod 11A57.
- Cosmos 201 - .
Mass: 6,300 kg (13,800 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Vostok.
Spacecraft: Zenit-4.
Duration: 8.00 days. Decay Date: 1968-02-14 . USAF Sat Cat: 3118 . COSPAR: 1968-009A. Apogee: 334 km (207 mi). Perigee: 207 km (128 mi). Inclination: 64.90 deg. Period: 89.90 min. High resolution photo reconnaissance satellite; returned film capsule.
1969 February 6 - .
- Volynov grounded - .
Nation: Russia.
Related Persons: Grechko, Andrei,
Kuznetsov, Nikolai F,
Leonov.
Program: Lunar L3.
Meetings are held at the cosmonaut centre to plan for the big visit to the base by Marshal Grechko. N F Kuznetsov briefs plans for the centre with the general staff. Kamanin discusses the situation with Leonov. Leonov notes the saying from Lenin on a banner at the centre: "Know how to work!" Unfortunately, they have left out the second part: "Don't hurry!" Leonov states he is not assigning Volynov to any future flights.
1969 February 6 - .
00:39 GMT - .
Launch Site:
Cape Canaveral.
Launch Complex:
Cape Canaveral LC17A.
LV Family:
Thor.
Launch Vehicle:
Thor Delta M.
1969 February 6 - .
06:31 GMT - .
Launch Site:
Tanegashima.
Launch Complex:
Tanegashima T.
Launch Vehicle:
LS-C.
- Test mission - .
Nation: Japan.
Agency: NASDA.
Apogee: 100 km (60 mi).
1969 February 6 - .
09:39 GMT - .
Launch Site:
Fort Churchill.
LV Family:
Deacon.
Launch Vehicle:
Nike Cajun.
- Grenades Aeronomy mission - .
Nation: USA.
Agency: NASA.
Apogee: 129 km (80 mi).
1969 February 6 - .
10:30 GMT - .
Launch Site:
Biscarosse.
LV Family:
Belier.
Launch Vehicle:
Dragon 2B.
- FU-180 Mass spectrometer F1 Ionosphere mission - .
Nation: France.
Agency: CNES.
Apogee: 430 km (260 mi).
1969 February 6 - .
13:45 GMT - .
Launch Site:
Biscarosse.
LV Family:
Belier.
Launch Vehicle:
Dragon 2B.
- FU-180 Mass spectrometer F2 Ionosphere mission - .
Nation: France.
Agency: CNES.
Apogee: 405 km (251 mi).
1969 February 6 - .
14:35 GMT - .
Launch Site:
Fort Churchill.
LV Family:
Aerobee.
Launch Vehicle:
Aerobee 150.
- Aeronomy mission - .
Nation: USA.
Agency: NASA.
Apogee: 138 km (85 mi).
1969 February 6 - .
17:09 GMT - .
Launch Site:
Wallops Island.
LV Family:
Deacon.
Launch Vehicle:
Nike Apache.
- Ionosphere mission - .
Nation: USA.
Agency: NASA.
Apogee: 219 km (136 mi).
1969 February 6 - .
19:29 GMT - .
Launch Site:
Wallops Island.
LV Family:
Deacon.
Launch Vehicle:
Nike Apache.
- Aeronomy mission - .
Nation: USA.
Agency: NASA.
Apogee: 117 km (72 mi).
1969 February 6 - .
21:09 GMT - .
Launch Site:
Wallops Island.
LV Family:
Deacon.
Launch Vehicle:
Nike Cajun.
- Aeronomy mission - .
Nation: USA.
Agency: NASA.
Apogee: 128 km (79 mi).
1969 February 6 - .
22:20 GMT - .
Launch Site:
Biscarosse.
LV Family:
Belier.
Launch Vehicle:
Dragon 2B.
- FU-180 Mass spectrometer F3 Ionosphere mission - .
Nation: France.
Agency: CNES.
Apogee: 430 km (260 mi).
1970 February 6 - .
1970 February 6 - .
04:16 GMT - .
Launch Site:
Baikonur.
Launch Complex:
Baikonur LC81/23.
Launch Pad: LC81/23?.
LV Family:
Proton.
Launch Vehicle:
Proton-K/D.
FAILURE: Failure of vehicle on launch..
Failed Stage: 1.
- Ye-8-5 s/n 405 - failure of vehicle on launch - .
Payload: Ye-8-5 s/n 405. Mass: 5,600 kg (12,300 lb). Nation: Russia.
Agency: RVSN.
Program: Luna.
Class: Moon.
Type: Lunar probe. Spacecraft Bus: Luna Ye-8.
Spacecraft: Luna Ye-8-5.
Decay Date: 1970-02-06 . Robotic lunar soil return mission..
1970 February 6 - .
16:30 GMT - .
Launch Site:
Cape Canaveral.
Launch Complex:
Cape Canaveral ETR.
Launch Platform: SSBN 626.
LV Family:
Polaris.
Launch Vehicle:
Polaris A3.
- Operational test - .
Nation: USA.
Agency: USN.
Apogee: 1,000 km (600 mi).
1970 February 6 - .
19:42 GMT - .
Launch Site:
Salto di Quirra.
LV Family:
Skylark.
Launch Vehicle:
Skylark 2 AC.
- ESRO S44 / 1 Stellar ultraviolet Ultraviolet astronomy mission - .
Nation: Europe.
Agency: ESRO.
Apogee: 211 km (131 mi).
1971 February 6 - .
- Incident with Shonin during DOS training. - .
Nation: Russia.
Related Persons: Shonin.
Program: Salyut.
Spacecraft Bus: Almaz.
Spacecraft: Salyut 1.
The training session at KIS yesterday was subverted by Shonin's drunkenness. Kamanin investigates the matter all day. Shonin is said to have brought vodka to the KIS and consumed vodka during the session. Kamanin confronted him, but of course he is sober now. Kamanin cannot understand the man, He has known him for eleven years and thought him a competent person.
1971 February 6 - .
1971 February 6 - .
08:11 GMT - .
1971 February 6 - .
18:30 GMT - .
Launch Site:
Salto di Quirra.
LV Family:
Skylark.
Launch Vehicle:
Skylark 3.
- ESRO S80 / 1 Ionosphere mission - .
Nation: Europe.
Agency: ESRO.
Apogee: 222 km (137 mi).
1971 February 6 - .
23:22 GMT - .
Launch Site:
Salto di Quirra.
LV Family:
Skylark.
Launch Vehicle:
Skylark 3.
- ESRO S80 / 2 Ionosphere mission - .
Nation: Europe.
Agency: ESRO.
Apogee: 226 km (140 mi).
1972 February 6 - .
06:35 GMT - .
Launch Site:
Tanegashima.
Launch Complex:
Tanegashima T.
Launch Vehicle:
JCR.
- Test mission - .
Nation: Japan.
Agency: NASDA.
Apogee: 200 km (120 mi).
1973 February 6 - .
10:35 GMT - .
Launch Site:
Poker Flat.
LV Family:
Tomahawk.
Launch Vehicle:
Nike Tomahawk.
- Caribou VII Aurora mission - .
Nation: USA.
Agency: Sandia.
Apogee: 270 km (160 mi).
1973 February 6 - .
19:59 GMT - .
Launch Site:
Andoya.
LV Family:
Tomahawk.
Launch Vehicle:
Nike Tomahawk.
- Ferdinand 30 / Electra-2 Plasma mission - .
Nation: USA.
Agency: NASA.
Apogee: 255 km (158 mi).
1974 February 6 - .
- Skylab 4 - Wakeup Song: Soul of Spain - .
Flight: Skylab 4.
"Soul of Spain" by 101 Strings.
1974 February 6 - .
Launch Site:
Vandenberg.
Launch Complex:
Vandenberg WTR.
Launch Platform: SSBN 598.
LV Family:
Polaris.
Launch Vehicle:
Polaris A3.
- Follow-on operational missile test - .
Nation: USA.
Agency: USN.
Apogee: 1,000 km (600 mi).
1974 February 6 - .
Launch Site:
Vandenberg.
Launch Complex:
Vandenberg WTR.
Launch Platform: SSBN 598.
LV Family:
Polaris.
Launch Vehicle:
Polaris A3.
- Follow-on operational missile test - .
Nation: USA.
Agency: USN.
Apogee: 1,000 km (600 mi).
1974 February 6 - .
Launch Site:
Vandenberg.
Launch Complex:
Vandenberg WTR.
Launch Platform: SSBN 598.
LV Family:
Polaris.
Launch Vehicle:
Polaris A3.
- Follow-on operational missile test - .
Nation: USA.
Agency: USN.
Apogee: 1,000 km (600 mi).
1974 February 6 - .
Launch Site:
Vandenberg.
Launch Complex:
Vandenberg WTR.
Launch Platform: SSBN 598.
LV Family:
Polaris.
Launch Vehicle:
Polaris A3.
- Follow-on operational missile test - .
Nation: USA.
Agency: USN.
Apogee: 1,000 km (600 mi).
1974 February 6 - .
Launch Site:
Vandenberg.
Launch Complex:
Vandenberg WTR.
Launch Platform: SSBN 598.
LV Family:
Polaris.
Launch Vehicle:
Polaris A3.
- Follow-on operational missile test - .
Nation: USA.
Agency: USN.
Apogee: 1,000 km (600 mi).
1974 February 6 - .
00:34 GMT - .
Launch Site:
Plesetsk.
Launch Complex:
Plesetsk LC132/2.
LV Family:
R-14.
Launch Vehicle:
Kosmos 11K65M.
- Cosmos 631 - .
Mass: 875 kg (1,929 lb). Nation: Russia.
Agency: MO.
Program: Tselina.
Class: Surveillance.
Type: SIGINT. Spacecraft: Tselina-O.
Decay Date: 1980-10-03 . USAF Sat Cat: 7109 . COSPAR: 1974-005A. Apogee: 545 km (338 mi). Perigee: 519 km (322 mi). Inclination: 74.00 deg. Period: 95.20 min. Replaced Cosmos 479. Possible ELINT satellite..
1974 February 6 - .
22:48 GMT - .
Launch Site:
Andoya.
LV Family:
Black Brant.
Launch Vehicle:
Black Brant IVB.
- DLR A-BB4-63 Auroral mission - .
Nation: Germany.
Agency: DFVLR.
Apogee: 548 km (340 mi).
1975 February 6 - .
Launch Site:
Poker Flat.
LV Family:
Black Brant.
Launch Vehicle:
Black Brant VI.
- Arctic test - .
Nation: USA.
Agency: US Army.
Apogee: 73 km (45 mi).
1975 February 6 - .
Launch Site:
Poker Flat.
LV Family:
Black Brant.
Launch Vehicle:
Black Brant VI.
- Arctic test - .
Nation: USA.
Agency: US Army.
Apogee: 69 km (42 mi).
1975 February 6 - .
04:49 GMT - .
Launch Site:
Plesetsk.
LV Family:
R-7.
Launch Vehicle:
Molniya 8K78M.
- Molniya 2-12 - .
Payload: Molniya-2. Mass: 1,600 kg (3,500 lb). Nation: Russia.
Agency: MOM.
Program: Molniya.
Class: Communications.
Type: Military communications satellite. Spacecraft Bus: KAUR-2.
Spacecraft: Molniya-2.
Decay Date: 1985-07-04 . USAF Sat Cat: 7641 . COSPAR: 1975-009A. Apogee: 40,746 km (25,318 mi). Perigee: 653 km (405 mi). Inclination: 62.80 deg. Period: 738.70 min. Decay date suspect Operation of the long-range telephone and telegraph radiocommunications system in the USSR; transmission of television programmes to stations in the Orbita network. .
1975 February 6 - .
16:35 GMT - .
Launch Site:
Kourou.
Launch Complex:
Kourou Diamant.
LV Family:
Diamant.
Launch Vehicle:
Diamant BP.4.
- Starlette - .
Payload: Starlette (BETA). Mass: 47 kg (103 lb). Nation: France.
Agency: CNES.
Class: Earth.
Type: Geodetic satellite. Spacecraft: Starlette.
USAF Sat Cat: 7646 . COSPAR: 1975-010A. Apogee: 1,108 km (688 mi). Perigee: 805 km (500 mi). Inclination: 49.80 deg. Period: 104.20 min. Geodesic satellite. .
1975 February 6 - .
22:04 GMT - .
Launch Site:
Cape Canaveral.
Launch Complex:
Cape Canaveral LC17B.
LV Family:
Thor.
Launch Vehicle:
Delta 2914.
1976 February 6 - .
Launch Site:
Vandenberg.
Launch Complex:
Vandenberg LF09.
Launch Pad: LF09?.
LV Family:
Minuteman.
Launch Vehicle:
Minuteman 3.
FAILURE: Failure.
- OT GT26GM-4 operational test launch - .
Nation: USA.
Agency: USAF SAC.
Apogee: 200 km (120 mi).
1977 February 6 - .
06:00 GMT - .
Launch Site:
Cape Canaveral.
Launch Complex:
Cape Canaveral LC40.
LV Family:
Titan.
Launch Vehicle:
Titan IIIC.
- IMEWS 7 - .
Payload: DSP Phase 2 s/n 9 / OPS 3151. Mass: 1,040 kg (2,290 lb). Nation: USA.
Agency: USAF.
Class: Surveillance.
Type: Early warning satellite. Spacecraft: DSP.
Completed Operations Date: 1984-01-01 . USAF Sat Cat: 9803 . COSPAR: 1977-007A. Apogee: 35,860 km (22,280 mi). Perigee: 35,620 km (22,130 mi). Inclination: 0.50 deg. Period: 1,433.30 min. Second generation geosynchronous ballistic missile launch detection satellite, remained in service for nearly seven years. Positioned in geosynchronous orbit over the Pacific Ocean at 135 deg W in 1977-1979; over the Indian Ocean 70 deg E in 1979-1984..
1977 February 6 - .
20:50 GMT - .
Launch Site:
Andoya.
LV Family:
Tomahawk.
Launch Vehicle:
Nike Tomahawk.
- Plasma mission - .
Nation: USA.
Agency: NASA.
Apogee: 224 km (139 mi).
1978 February 6 - .
00:20 GMT - .
Launch Site:
South Uist.
Launch Vehicle:
Petrel.
- Ultraviolet airglow Atmospheric mission - .
Nation: UK.
Agency: SRC.
Apogee: 136 km (84 mi).
1978 February 6 - .
01:00 GMT - .
Launch Site:
South Uist.
Launch Vehicle:
Petrel.
- La / ne Ionosphere mission - .
Nation: UK.
Agency: SRC.
Apogee: 125 km (77 mi).
1978 February 6 - .
18:55 GMT - .
Launch Site:
Syowa Base.
Launch Vehicle:
S-210.
- Aurora mission - .
Nation: Japan.
Agency: NIPR.
Apogee: 116 km (72 mi).
1979 February 6 - .
Launch Site:
Malmstrom AFB.
LV Family:
Minuteman.
Launch Vehicle:
Minuteman 3.
- Malmstrom AFB - .
The integrated program of improvements to Minuteman ground systems was completed at Wing I and the sites were returned to the custody of SAC..
1979 February 6 - .
Launch Site:
Vandenberg.
Launch Complex:
Vandenberg LF26.
Launch Pad: LF26?.
LV Family:
Minuteman.
Launch Vehicle:
Minuteman 3.
- FOT GT67GB Follow-on Test launch - .
Nation: USA.
Agency: USAF SAC.
Apogee: 1,300 km (800 mi).
1979 February 6 - .
08:46 GMT - .
Launch Site:
Tanegashima.
Launch Complex:
Tanegashima N.
LV Family:
Thor.
Launch Vehicle:
N-1.
FAILURE: Third stage collided with ECS a..
Failed Stage: 3.
- Ayame 1 - .
Payload: ECS a; ECS 1. Mass: 260 kg (570 lb). Nation: Japan.
Agency: NASDA.
Class: Technology.
Type: Communications technology satellite. Spacecraft: Ayame.
Completed Operations Date: 1979-02-09 . USAF Sat Cat: 11261 . COSPAR: 1979-009A. Apogee: 37,278 km (23,163 mi). Perigee: 29,407 km (18,272 mi). Inclination: 5.60 deg. Period: 1,313.10 min.
Experimental Communications Satellite. Experimental Communications Satellite (ECS). Launch time 0846 GMT. ECS was injected into the planned transfer orbit. On 9 Feb, however, ECS ceased radio transmissions about 10 seconds after the apogee kick motor was fired. Communicat ions and propagation experiments of satellite-communication systems. Operation and control experiment for geostationary satellites. Mass at launch 260 kg. Configuration - cylindrical. Height 1.9m including antenna. Diameter 1.4m. Spin stabilized. Last known longitude (13 June 1995) 146.23 deg W drifting at 33.817 deg E per day.
1980 February 6 - .
Launch Site:
Grand Turk Island.
Launch Complex:
Grand Turk Island DZ.
Launch Pad: Aircraft from Cape Canaveral.
Launch Platform: B-52.
Launch Vehicle:
SRAM.
- Test mission - .
Nation: USA.
Agency: USAF.
Apogee: 10 km (6 mi).
1981 February 6 - .
08:00 GMT - .
Launch Site:
Plesetsk.
Launch Complex:
Plesetsk LC132/1.
LV Family:
R-14.
Launch Vehicle:
Kosmos 11K65M.
- Intercosmos 21 - .
Payload: AUOS-Z-R-P-IK. Mass: 550 kg (1,210 lb). Nation: Russia.
Agency: IK.
Manufacturer: Yuzhnoye.
Program: Intercosmos.
Class: Technology.
Type: Navigation technology satellite. Spacecraft: AUOS.
Completed Operations Date: 1982-06-02 . Decay Date: 1982-07-07 . USAF Sat Cat: 12162 . COSPAR: 1981-011A. Apogee: 506 km (314 mi). Perigee: 469 km (291 mi). Inclination: 74.00 deg. Period: 94.40 min.
Oceanographic, terrestrial studies. Development of methods for comprehensive study of the oceans and the surface of the earth, and testing of the experimental system of automatic gathering of scientific information from sea and land stations. Launched under the INTERCOSMOS programme by the USSR together with the Czechoslovak Socialist Republic, the German Democratic Republic, the Hungarian People's Republic and the Socialist Republic of Romania.
1983 February 6 - .
11:31 GMT - .
Launch Site:
Baikonur.
Launch Complex:
Baikonur LC31.
LV Family:
R-7.
Launch Vehicle:
Soyuz-U.
- Cosmos 1439 - .
Payload: Yantar-2K s/n 956. Mass: 6,600 kg (14,500 lb). Nation: Russia.
Agency: MOM.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft Bus: Yantar.
Spacecraft: Yantar-2K.
Duration: 16.00 days. Decay Date: 1983-02-22 . USAF Sat Cat: 13784 . COSPAR: 1983-007A. Apogee: 344 km (213 mi). Perigee: 168 km (104 mi). Inclination: 70.40 deg. Period: 89.60 min. Area survey photo reconnaissance; film capsule; also performed earth resources tasks. Returned in less than usual 30 day full duration..
1984 February 6 - .
Launch Site:
San Clemente.
Launch Complex:
San Clemente E.
Launch Vehicle:
Dolphin.
FAILURE: Nitrogen gas fittings had been loosened during transport. Attempts to grind an access hole to an internal bay of the rocket to tighten the fittings resulted in a fire in the electronics..
- Dolphin hybrid rocket sea-launch abort. - .
Nation: USA.
Agency: Starstruck.
The Dolphin included not only innovative hybrid propulsion technology but was also launched from a floating launch cannister at sea. This was the first attempted test of the sea-launch system, although the launch itself was aborted..
1984 February 6 - .
- STS-41-B - Wakeup Song: Glory, Glory, Colorado - .
Flight: STS-41-B.
"Glory, Glory, Colorado" by the University of Colorado Band. That's the fight song of that institution which is Vance Brand's alma mater followed by"Ride High You Mustangs" the Cal Poly State University fight song which is Pilot Robert Gibson's alma mater.
1985 February 6 - .
Launch Site:
Vandenberg.
Launch Complex:
Vandenberg.
LV Family:
Atlas.
Launch Vehicle:
Atlas F.
1985 February 6 - .
Launch Site:
Vandenberg.
Launch Complex:
Vandenberg LF04.
LV Family:
Minuteman.
Launch Vehicle:
Minuteman 3.
FAILURE: Failure.
- FOT GT106GM Follow-on Test launch - .
Nation: USA.
Agency: USAF SAC.
Apogee: 100 km (60 mi).
1985 February 6 - .
11:00 GMT - .
Launch Site:
Plesetsk.
LV Family:
R-7.
Launch Vehicle:
Soyuz-U.
- Cosmos 1628 - .
Mass: 6,300 kg (13,800 lb). Nation: Russia.
Agency: MOM.
Class: Earth.
Type: Earth resources satellite. Spacecraft Bus: Vostok.
Spacecraft: Zenit-8.
Duration: 14.00 days. Decay Date: 1985-02-20 . USAF Sat Cat: 15514 . COSPAR: 1985-012A. Apogee: 378 km (234 mi). Perigee: 191 km (118 mi). Inclination: 72.90 deg. Period: 90.20 min. Military cartographic satellite; returned film capsule..
1985 February 6 - .
21:45 GMT - .
Launch Site:
Plesetsk.
Launch Complex:
Plesetsk LC32.
Launch Pad: LC32/1.
LV Family:
R-36.
Launch Vehicle:
Tsiklon-3.
- Meteor 2-12 - .
Payload: Meteor-2 no. 12. Mass: 2,750 kg (6,060 lb). Nation: Russia.
Agency: MO.
Class: Earth.
Type: Weather satellite. Spacecraft Bus: Meteor.
Spacecraft: Meteor-2.
USAF Sat Cat: 15516 . COSPAR: 1985-013A. Apogee: 958 km (595 mi). Perigee: 932 km (579 mi). Inclination: 82.50 deg. Period: 104.00 min. Gathering meteorological information and data on penetrating radiation fluxes in circumterrestrial space. .
1986 February 6 - .
Launch Site:
Sriharikota.
LV Family:
RH.
Launch Vehicle:
RH-200.
- Meteorological Chaff Meteorological mission - .
Nation: India.
Agency: ISRO.
Apogee: 70 km (43 mi).
1988 February 6 - .
20:40 GMT - .
Launch Site:
Cape Canaveral.
Launch Complex:
Cape Canaveral LC47.
LV Family:
Deacon.
Launch Vehicle:
Rocketsonde.
- Arcasonde - .
Nation: USA.
Agency: MRN.
Apogee: 66 km (41 mi).
1990 February 6 - .
Launch Site:
Vandenberg.
Launch Complex:
Vandenberg LF26.
Launch Pad: LF26?.
LV Family:
Minuteman.
Launch Vehicle:
Minuteman 3.
- FOT GT137GB Follow-on Test launch - .
Nation: USA.
Agency: USAF SAC.
Apogee: 1,300 km (800 mi).
1990 February 6 - .
16:30 GMT - .
Launch Site:
Plesetsk.
Launch Complex:
Plesetsk LC132/2.
LV Family:
R-14.
Launch Vehicle:
Kosmos 11K65M.
- Cosmos 2059 - .
Mass: 500 kg (1,100 lb). Nation: Russia.
Agency: MO.
Class: Surveillance.
Type: Radar calibration target. Spacecraft Bus: AUOS.
Spacecraft: Taifun-2.
Decay Date: 1990-11-12 . USAF Sat Cat: 20476 . COSPAR: 1990-012A. Apogee: 1,585 km (984 mi). Perigee: 184 km (114 mi). Inclination: 65.80 deg. Period: 102.70 min. Released 10 Romb radar calibration subsatellites..
1991 February 6 - .
- Salyut-7 Burnup In Earth's Atmosphere (Soviet Union Space Station) - .
Nation: Russia.
Spacecraft Bus: Almaz.
Spacecraft: Salyut 7.
1991 February 6 - .
07:29 GMT - .
Launch Site:
Wallops Island.
LV Family:
Talos.
Launch Vehicle:
Space Data LCLV.
- Target / active plasma mission - .
Nation: USA.
Agency: OSC.
Type: ABM Target. Apogee: 510 km (310 mi).
1994 February 6 - .
- STS-60 - Wakeup Song: The Bug - .
Flight: STS-60.
"The Bug" by Mary Chapin Carpenter.
1995 February 6 - .
- STS-63 - Wakeup Song: Make New Friends - .
Flight: STS-63.
"Make New Friends" From a Girl Scout Brownie troop (the daughter of the people who send flowers to MCC each mission is in the troop).
1998 February 6 - .
17:18 GMT - .
Launch Site:
Rothera.
LV Family:
Viper.
Launch Vehicle:
Viper 3A.
- TPS16 Aeronomy mission - .
Nation: UK.
Agency: DLR.
Apogee: 100 km (60 mi).
2000 February 6 - .
16:37 GMT - .
Launch Site:
Alcantara.
LV Family:
Sonda.
Launch Vehicle:
VS-30.
- Lencois Maranhenses Microgravity mission - .
Nation: Brazil.
Agency: AEB.
Apogee: 148 km (91 mi).
2002 February 6 - .
09:38 GMT - .
Launch Site:
Poker Flat.
LV Family:
Black Brant.
Launch Vehicle:
Black Brant XII.
- RACE Ionosphere mission - .
Nation: USA.
Agency: NASA.
Apogee: 922 km (572 mi).
2002 February 6 - .
10:30 GMT - .
Launch Site:
Kagoshima.
Launch Complex:
Kagoshima L.
Launch Pad: K.
Launch Vehicle:
S-310.
- NTV-2 Thermosphere Aeronomy mission - .
Nation: Japan.
Agency: ISAS.
Apogee: 150 km (90 mi).
2003 February 6 - .
07:30 GMT - .
Launch Site:
White Sands.
LV Family:
Black Brant.
Launch Vehicle:
Black Brant IX.
- NUVIEWS 3 Ultraviolet astronomy mission - .
Nation: USA.
Agency: NASA Greenbelt.
Apogee: 300 km (180 mi).
2003 February 6 - .
21:00 GMT - .
Launch Site:
Vandenberg.
Launch Complex:
Vandenberg 576E.
LV Family:
Pegasus.
Launch Vehicle:
GBI.
- BV-6 Boost Vehicle Test Flight - .
Nation: USA.
Agency: USAF AFSPC.
Manufacturer: OSC.
Apogee: 1,810 km (1,120 mi).
Successful first launch of the prototype of the three-stage version of the Taurus launch vehicle being developed by Orbital Sciences for Boeing for use in the Ground-based Midcourse Defense (GMD) system. The vehicle launched the dummy payload on a trajectory over the Pacific Ocean, reaching an altitude of 2100 km and traveling 6500 km down range.
2004 February 6 - .
- International Space Station Status Report #04-8 - .
Nation: USA.
Related Persons: Foale,
Kaleri.
Program: ISS.
Flight: Soyuz TMA-3.
Aboard the International Space Station, Mike Foale and Alexander Kaleri of the Expedition 8 crew spent this week unpacking the first fresh supplies to arrive at the complex since they began their mission more than three and a half months ago..
Additional Details: here....
2006 February 6 - .
Launch Site:
Xichang.
Launch Vehicle:
DF-21.
- ASAT - .
Nation: China.
Agency: PRC.
Apogee: 850 km (520 mi).
2008 February 6 - .
2009 February 6 - .
10:22 GMT - .
Launch Site:
Vandenberg.
Launch Complex:
Vandenberg SLC2W.
LV Family:
Thor.
Launch Vehicle:
Delta 7320-10C.
- NOAA 19 - .
Payload: NOAA-O. Mass: 1,420 kg (3,130 lb). Nation: USA.
Agency: NOAA.
Manufacturer: Lockheed.
Program: Tiros.
Class: Earth.
Type: Weather satellite. Spacecraft: Advanced Tiros N.
USAF Sat Cat: 33591 . COSPAR: 2009-005A. Apogee: 867 km (538 mi). Perigee: 845 km (525 mi). Inclination: 98.80 deg. Period: 102.10 min.
2011 February 6 - .
12:26 GMT - .
Launch Site:
Vandenberg.
Launch Complex:
Vandenberg SLC8.
LV Family:
Minuteman.
Launch Vehicle:
Minotaur 1.
- USA 225 - .
Payload: RPP. Mass: 235 kg (518 lb). Nation: USA.
Class: Technology.
Type: Technology satellite. Spacecraft Bus: Aquila-M1.
Spacecraft: RPP.
USAF Sat Cat: 37364 . COSPAR: 2011-006A. National Reconnaissance Office Rapid Pathfinder Program technology satellite, probably placed in polar orbit. Built in less than two years for under $20 million to test classified sensors..
2013 February 6 - .
16:04 GMT - .
Launch Site:
Baikonur.
Launch Complex:
Baikonur LC31.
Launch Pad: LC31/6.
LV Family:
R-7.
Launch Vehicle:
Soyuz-2-1A.
- Globalstar M097 - .
Mass: 700 kg (1,540 lb). Nation: USA.
Class: Communications.
Type: Communications satellite. Spacecraft: Proteus.
USAF Sat Cat: 39072 . COSPAR: 2013-005A. Apogee: 1,414 km (878 mi). Perigee: 1,413 km (877 mi). Inclination: 52.00 deg. Period: 114.08 min.
- Globalstar M093 - .
Mass: 700 kg (1,540 lb). Nation: USA.
Class: Communications.
Type: Communications satellite. Spacecraft: Proteus.
USAF Sat Cat: 39073 . COSPAR: 2013-005B. Apogee: 1,414 km (878 mi). Perigee: 1,413 km (877 mi). Inclination: 51.98 deg. Period: 114.08 min.
- Globalstar M094 - .
Mass: 700 kg (1,540 lb). Nation: USA.
Class: Communications.
Type: Communications satellite. Spacecraft: Proteus.
USAF Sat Cat: 39074 . COSPAR: 2013-005C. Apogee: 927 km (576 mi). Perigee: 916 km (569 mi). Inclination: 52.01 deg. Period: 103.44 min.
- Globalstar M096 - .
Mass: 700 kg (1,540 lb). Nation: USA.
Class: Communications.
Type: Communications satellite. Spacecraft: Proteus.
USAF Sat Cat: 39075 . COSPAR: 2013-005D. Apogee: 1,415 km (879 mi). Perigee: 1,413 km (877 mi). Inclination: 52.00 deg. Period: 114.08 min.
- Globalstar M078 - .
Mass: 700 kg (1,540 lb). Nation: USA.
Class: Communications.
Type: Communications satellite. Spacecraft: Proteus.
USAF Sat Cat: 39076 . COSPAR: 2013-005E. Apogee: 1,414 km (878 mi). Perigee: 1,413 km (877 mi). Inclination: 51.99 deg. Period: 114.08 min.
- Globalstar M095 - .
Mass: 700 kg (1,540 lb). Nation: USA.
Class: Communications.
Type: Communications satellite. Spacecraft: Proteus.
USAF Sat Cat: 39077 . COSPAR: 2013-005F. Apogee: 1,414 km (878 mi). Perigee: 1,413 km (877 mi). Inclination: 51.98 deg. Period: 114.08 min. Six satellites in one launch; replenishment of Globalstar MEO mobile-phone communications satellite constellation..
2014 February 6 - .
21:30 GMT - .
Launch Site:
Kourou.
Launch Complex:
Kourou ELA3.
LV Family:
Ariane 5.
Launch Vehicle:
Ariane 5ECA.
- ABS 2 - .
Mass: 6,330 kg (13,950 lb). Nation: China.
Class: Communications.
Type: Communications satellite. Spacecraft: FS-1300.
USAF Sat Cat: 39508 . COSPAR: 2014-006A. Apogee: 35,801 km (22,245 mi). Perigee: 35,772 km (22,227 mi). Inclination: 0.0300 deg. Period: 1,436.10 min.
Communications satellite for Hong-Kong-based Asia Broadcast Satellite. Stationed at 75 deg E, serving four continents: 6 dedicated high powered Ku-band beams for DTH services in the Eastern Hemisphere; C-band beams for Africa and SE Asia connectivity requirements; Ka-band beam targeting the MENA region for commercial and military applications.
- Athena-Fidus - .
Payload: Spacebus-4000B2. Mass: 3,080 kg (6,790 lb). Nation: France.
Spacecraft: Spacebus 4000.
USAF Sat Cat: 39509 . COSPAR: 2014-006B. Apogee: 35,792 km (22,240 mi). Perigee: 35,781 km (22,233 mi). Inclination: 0.0600 deg. Period: 1,436.10 min.
Joint French/Italian military communications satellite for both military and civilian government communications; in France the civilian space agency CNES and the military procurement agency DGA were both responsible, while in Italy the corresponding Agenzia Spaziale Italiana and Segredifesa/DNA agencies were involved.
2018 February 6 - .
03:00 GMT - .
Launch Site:
Kalam Island.
LV Family:
ASLV.
Launch Vehicle:
Agni 1.
- Agni RV - .
Nation: India.
Apogee: 300 km (180 mi). Test mission. Impacted Bay of Bengal..
2018 February 6 - .
20:44 GMT - .
Launch Site:
Cape Canaveral.
Launch Complex:
Cape Canaveral LC39A.
LV Family:
Falcon.
Launch Vehicle:
Falcon 9 Heavy.
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