Baikonur LC175/2
Site · Russia
Original archive entry. The text, images and links below are kept as they were written.
UR-100N launch complex.
Related
- Country
- Russia
- Spacecraft
- Kondor
- Launch Vehicles
- UR-100NU 15A35, Rokot, Strela launch vehicle
- Launch Sites
- Baikonur
Chronology
11 events
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.1999 October 20
Launch Site: Baikonur. Launch Complex: Baikonur LC175/2. Launch Pad: LC175/pad?. LV Family: UR-100N. Launch Vehicle: UR-100NU 15A35.2000 November 1
10:00 GMT - . Launch Site: Baikonur. Launch Complex: Baikonur LC175/2. LV Family: UR-100N. Launch Vehicle: UR-100NU 15A35.2001 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 15A35.2003 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 15A35.2006 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 15A35.2008 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..