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SJ-7
SJ-7 Credit: Manufacturer Image |
Chinese maneuverable military satellites, believed to have an interceptor / inspector / antisatellite mission. Launched from Jiuquan by the CZ-2D launch vehicle into 600 km, 97.7 deg inclination sun synchronous orbits.
Status: Operational 2005. First Launch: 2005-07-05. Last Launch: 2010-06-15. Number: 2 .
The second carried out a close pass or even came in contact with the SJ-6/3A satellite on 19 August 2010.
More at: SJ-7.
Family:
Military.
Country:
China.
Launch Vehicles:
Chang Zheng 2D.
Launch Sites:
Jiuquan SLS-2.
Bibliography:
13103.
2005 July 5 - .
22:40 GMT - .
Launch Site:
Jiuquan.
Launch Complex:
Jiuquan SLS-2.
Launch Pad: Pad 603.
LV Family:
CZ.
Launch Vehicle:
Chang Zheng 2D.
- SJ-7 - .
Payload: Shi Jian 7. Mass: 2,000 kg (4,400 lb). Nation: China.
Manufacturer: CASC.
Spacecraft: SJ-7.
USAF Sat Cat: 28737 . COSPAR: 2005-024A. Apogee: 573 km (356 mi). Perigee: 555 km (344 mi). Inclination: 97.60 deg. Period: 95.90 min. Perhaps early test of satellite inspector/interceptor hardware; orbit similar to SJ-12 in 2010..
2010 June 15 - .
01:39 GMT - .
Launch Site:
Jiuquan.
LV Family:
CZ.
Launch Vehicle:
Chang Zheng 2D.
- SJ-12 - .
Nation: China.
Agency: SISE.
Class: Military.
Type: Anti-satellite system. Spacecraft: SJ-7.
USAF Sat Cat: 36596 . COSPAR: 2010-027A. Apogee: 602 km (374 mi). Perigee: 578 km (359 mi). Inclination: 97.70 deg. Period: 96.50 min. Satellite inspector/interceptor. Carried out a close pass or even came in contact with the SJ-6/3A satellite on 19 August 2010. By 21 September was in a 580 km x 606 km x 97.8 deg orbit..
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