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APT Satellite Company
Chinese agency. APT Satellite Company (Asia Pacific Telecom), Hong Kong, China.
AKA: APT. Number: 4 . Duration: 35.30 days. Location: Hong Kong.
Country:
China.
Spacecraft:
Apstar.
1994 July 21 - .
10:55 GMT - .
Launch Site:
Xichang.
Launch Complex:
Xichang LC1.
LV Family:
CZ.
Launch Vehicle:
Chang Zheng 3.
- Apstar 1 - .
Mass: 1,383 kg (3,048 lb). Nation: China.
Agency: APT Satellite Company.
Program: Apstar.
Class: Communications.
Type: Civilian communications satellite. Spacecraft: HS 376.
USAF Sat Cat: 23185 . COSPAR: 1994-043A. Apogee: 35,789 km (22,238 mi). Perigee: 35,785 km (22,235 mi). Inclination: 0.00 deg. Period: 1,436.12 min. Asia-Pacific communications. Operated in geosynchronous orbit at 138 deg E in 1994-1999. As of 5 September 2001 located at 138.04 deg E drifting at 0.004 deg W per day. As of 2007 Mar 11 located at 141.96E drifting at 0.002W degrees per day..
1996 July 3 - .
10:47 GMT - .
Launch Site:
Xichang.
Launch Complex:
Xichang LC1.
LV Family:
CZ.
Launch Vehicle:
Chang Zheng 3.
- Apstar 1A - .
Mass: 2,800 kg (6,100 lb). Nation: China.
Agency: APT Satellite Company.
Program: Apstar.
Class: Communications.
Type: Civilian communications satellite. Spacecraft: HS 376.
USAF Sat Cat: 23943 . COSPAR: 1996-039A. Apogee: 35,791 km (22,239 mi). Perigee: 35,785 km (22,235 mi). Inclination: 0.00 deg. Period: 1,436.10 min. 24 C-band transponders; Operated in geosynchronous orbit at 134 deg E in 1996-1999. As of 6 September 2001 located at 134.02 deg E drifting at 0.013 deg W per day. As of 2007 Mar 10 located at 129.99E drifting at 0.007E degrees per day..
1997 October 16 - .
19:13 GMT - .
Launch Site:
Xichang.
Launch Complex:
Xichang LC2.
LV Family:
CZ.
Launch Vehicle:
Chang Zheng 3B.
- Apstar 2R - .
Mass: 3,700 kg (8,100 lb). Nation: China.
Agency: APT Satellite Company.
Manufacturer: Palo Alto.
Program: Apstar.
Class: Communications.
Type: Civilian communications satellite. Spacecraft: FS-1300.
USAF Sat Cat: 25010 . COSPAR: 1997-062A. Apogee: 35,798 km (22,243 mi). Perigee: 35,774 km (22,228 mi). Inclination: 0.00 deg. Period: 1,436.10 min. Geosynchronous. Stationed over 76.5E Positioned in geosynchronous orbit at 76 deg E in 1997-1999 As of 5 September 2001 located at 76.48 deg E drifting at 0.001 deg W per day. As of 2007 Mar 11 located at 76.46E drifting at 0.002W degrees per day..
2004 June 29 - .
03:58 GMT - .
Launch Site:
Kiritimati.
Launch Pad: 0.0 N x 154.0 W.
Launch Platform: Odyssey.
LV Family:
Zenit.
Launch Vehicle:
Zenit-3SL.
FAILURE: Partial failure - upper stage left satellite stranded in useless orbit..
Failed Stage: 3.
- Apstar 5 - .
Payload: Apstar 1R, Telstar 18, LS-1300. Mass: 4,640 kg (10,220 lb). Nation: China.
Agency: APT Satellite Company.
Manufacturer: Palo Alto.
Program: Apstar.
Class: Communications.
Type: Civilian communications satellite. Spacecraft: FS-1300.
USAF Sat Cat: 28364 . COSPAR: 2004-024A. Apogee: 35,799 km (22,244 mi). Perigee: 35,775 km (22,229 mi). Inclination: 0.10 deg. Period: 1,436.10 min. Delayed from November 2003, April 28 2004. Partial failure (upper stage). As of 2007 Mar 11 located at 138.01E drifting at 0.009W degrees per day..
2005 April 12 - .
12:00 GMT - .
Launch Site:
Xichang.
Launch Complex:
Xichang LC2.
LV Family:
CZ.
Launch Vehicle:
Chang Zheng 3B.
- Apstar 6 - .
Payload: Apstar 5B / Spacebus 4000C2. Mass: 4,680 kg (10,310 lb). Nation: China.
Agency: APT Satellite Company.
Program: Apstar.
Class: Communications.
Type: Civilian communications satellite. Spacecraft: Spacebus 4000.
USAF Sat Cat: 28638 . COSPAR: 2005-012A. Apogee: 35,795 km (22,241 mi). Perigee: 35,778 km (22,231 mi). Inclination: 0.0200 deg. Period: 1,436.09 min. Delayed from November, December 4, 2004. Ku and C band transponders. As of 2007 Mar 11 located at 133.99E drifting at 0.013W degrees per day..
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