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Baikonur LC175/2
Part of Baikonur
UR-100N launch complex.
Longitude: 62.99 deg. Latitude: 46.05 deg.
Country:
Russia.
Spacecraft:
Kondor.
Launch Vehicles:
UR-100NU 15A35,
Rokot,
Strela launch vehicle.
Launch Sites:
Baikonur.
1991 December 20 - .
21:31 GMT - .
Launch Site:
Baikonur.
Launch Complex:
Baikonur LC175/2.
Launch Pad: LC175/58.
LV Family:
UR-100N.
Launch Vehicle:
Rokot.
- Grand Prix test - .
Nation: Russia.
Agency: VKS.
Apogee: 1,000 km (600 mi).
1999 October 20 - .
Launch Site:
Baikonur.
Launch Complex:
Baikonur LC175/2.
Launch Pad: LC175/pad?.
LV Family:
UR-100N.
Launch Vehicle:
UR-100NU 15A35.
- Operational missile test - .
Nation: Russia.
Agency: RVSN.
Apogee: 1,000 km (600 mi).
2000 November 1 - .
10:00 GMT - .
Launch Site:
Baikonur.
Launch Complex:
Baikonur LC175/2.
LV Family:
UR-100N.
Launch Vehicle:
UR-100NU 15A35.
- Operational missile test - .
Nation: Russia.
Agency: RVSN.
Apogee: 1,000 km (600 mi).
2001 October 26 - .
12:33 GMT - .
Launch Site:
Baikonur.
Launch Complex:
Baikonur LC175/2.
Launch Pad: LC175/pad?.
LV Family:
UR-100N.
Launch Vehicle:
UR-100NU 15A35.
- Operational missile test - .
Nation: Russia.
Agency: RVSN.
Apogee: 1,000 km (600 mi).
2003 December 5 - .
06:00 GMT - .
Launch Site:
Baikonur.
Launch Complex:
Baikonur LC175/2.
LV Family:
UR-100N.
Launch Vehicle:
Strela launch vehicle.
- Payload Mockup - .
Nation: Russia.
Agency: KVR.
Decay Date: 2015-12-15 . USAF Sat Cat: 28098 . COSPAR: 2003-055A. Apogee: 460 km (280 mi). Perigee: 454 km (282 mi). Inclination: 67.10 deg. Period: 93.70 min. Originally reported as an ICBM test. A Reuters story, later confirmed, claimed it was the first orbital launch of the Strela version of the rocket..
2005 October 20 - .
07:30 GMT - .
Launch Site:
Baikonur.
Launch Complex:
Baikonur LC175/2.
Launch Pad: LC175/pad?.
LV Family:
UR-100N.
Launch Vehicle:
UR-100NU 15A35.
- OT Kura - .
Nation: Russia.
Agency: RVSN.
Apogee: 1,000 km (600 mi).
2006 November 9 - .
11:35 GMT - .
Launch Site:
Baikonur.
Launch Complex:
Baikonur LC175/2.
Launch Pad: LC175/pad?.
LV Family:
UR-100N.
Launch Vehicle:
UR-100NU 15A35.
- Operational missile test - .
Nation: Kazakhstan.
Agency: RVSN.
Apogee: 1,000 km (600 mi).
2007 October 29 - .
09:00 GMT - .
Launch Site:
Baikonur.
Launch Complex:
Baikonur LC175/2.
Launch Pad: LC175/pad?.
LV Family:
UR-100N.
Launch Vehicle:
UR-100NU 15A35.
- Operational test - .
Nation: Russia.
Agency: RVSN.
Apogee: 1,000 km (600 mi).
2008 October 22 - .
09:10 GMT - .
Launch Site:
Baikonur.
Launch Complex:
Baikonur LC175/2.
LV Family:
UR-100N.
Launch Vehicle:
UR-100NU 15A35.
- Kura OT - .
Nation: Russia.
Apogee: 1,000 km (600 mi).
2013 June 27 - .
16:53 GMT - .
Launch Site:
Baikonur.
Launch Complex:
Baikonur LC175/2.
LV Family:
UR-100N.
Launch Vehicle:
Strela launch vehicle.
- Cosmos 2487 - .
Mass: 1,000 kg (2,200 lb). Nation: Russia.
Class: Earth.
Type: Civilian Radarsat. Spacecraft: Kondor.
USAF Sat Cat: 39194 . COSPAR: 2013-032A. Apogee: 501 km (311 mi). Perigee: 497 km (308 mi). Inclination: 74.73 deg. Period: 94.60 min.
First Kondor satellite, part of a new system of optical and radar military surveillance satellites; payload on this mission reportedly an S-band synthetic apperture radar with a swath width of 10 km and ground resolution of 1 m in spotlight mode, 3 m in stripmap mode, and 5-30 m in ScanSAR mode.
2014 December 19 - .
04:43 GMT - .
Launch Site:
Baikonur.
Launch Complex:
Baikonur LC175/2.
Launch Pad: Baikonur LC175.
LV Family:
UR-100N.
Launch Vehicle:
Strela launch vehicle.
- Kondor-E No. 2 - .
Mass: 1,100 kg (2,400 lb). Nation: South Africa.
Class: Surveillance.
Type: Civilian Radarsat. Spacecraft: Kondor.
USAF Sat Cat: 40353 . COSPAR: 2014-084A. Apogee: 484 km (300 mi). Perigee: 481 km (298 mi). Inclination: 74.75 deg. Period: 94.26 min. Second Kondor radar imaging satellite built by NPO Mashinostroenie (Moscow/Reutov)This satellite was the export version of the spacecraft and was reportedly sold to the Defense Intelligence organization of the South African National Defense Force..
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