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Baikonur LC191/66
Part of Baikonur
FOBS launch site.
First Launch: 1969-09-15. Last Launch: 1971-08-08. Number: 4 . Longitude: 63.20 deg. Latitude: 45.97 deg.
Country:
Russia.
Spacecraft:
OGCh.
Launch Vehicles:
R-36O 8K69,
R-36O 8K69M.
Launch Sites:
Baikonur.
1969 September 15 - .
16:05 GMT - .
Launch Site:
Baikonur.
Launch Complex:
Baikonur LC191/66.
LV Family:
R-36.
Launch Vehicle:
R-36O 8K69.
- Cosmos 298 - .
Mass: 1,700 kg (3,700 lb). Nation: Russia.
Agency: RVSN.
Class: Military.
Type: Orbital bombing system. Spacecraft: OGCh.
Decay Date: 1969-09-15 . USAF Sat Cat: 4092 . COSPAR: 1969-077A. Apogee: 162 km (100 mi). Perigee: 127 km (78 mi). Inclination: 49.60 deg. Period: 87.30 min. Fractional Orbital Bombardment System test..
1970 July 28 - .
22:00 GMT - .
Launch Site:
Baikonur.
Launch Complex:
Baikonur LC191/66.
LV Family:
R-36.
Launch Vehicle:
R-36O 8K69.
- Cosmos 354 - .
Mass: 1,700 kg (3,700 lb). Nation: Russia.
Agency: RVSN.
Class: Military.
Type: Orbital bombing system. Spacecraft: OGCh.
Decay Date: 1970-07-28 . USAF Sat Cat: 4481 . COSPAR: 1970-056A. Apogee: 165 km (102 mi). Perigee: 137 km (85 mi). Inclination: 49.60 deg. Period: 87.50 min. Fractional Orbital Bombardment System test..
1970 September 25 - .
14:05 GMT - .
Launch Site:
Baikonur.
Launch Complex:
Baikonur LC191/66.
LV Family:
R-36.
Launch Vehicle:
R-36O 8K69M.
- Cosmos 365 - .
Mass: 1,700 kg (3,700 lb). Nation: Russia.
Agency: RVSN.
Class: Military.
Type: Orbital bombing system. Spacecraft: OGCh.
Decay Date: 1970-09-25 . USAF Sat Cat: 4556 . COSPAR: 1970-076A. Apogee: 173 km (107 mi). Perigee: 145 km (90 mi). Inclination: 49.50 deg. Period: 87.70 min. Fractional Orbital Bombardment System test..
1971 August 8 - .
23:45 GMT - .
Launch Site:
Baikonur.
Launch Complex:
Baikonur LC191/66.
LV Family:
R-36.
Launch Vehicle:
R-36O 8K69M.
- Cosmos 433 - .
Mass: 1,700 kg (3,700 lb). Nation: Russia.
Agency: RVSN.
Class: Military.
Type: Orbital bombing system. Spacecraft: OGCh.
Decay Date: 1971-08-09 . USAF Sat Cat: 5402 . COSPAR: 1971-068A. Apogee: 299 km (185 mi). Perigee: 112 km (69 mi). Inclination: 49.40 deg. Period: 88.50 min. Fractional Orbital Bombardment System test..
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