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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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