Baikonur LC191/66
Site · Russia
Original archive entry. The text, images and links below are kept as they were written.
FOBS launch site.
Related
- Country
- Russia
- Spacecraft
- OGCh
- Launch Vehicles
- R-36O 8K69, R-36O 8K69M
- Launch Sites
- Baikonur
Chronology
4 events
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..