Encyclopedia Astronautica
Chinasat


More... - Chronology...

Chinasat Chronology


1991 December 28 - . 12:00 GMT - . Launch Site: Xichang. Launch Complex: Xichang LC1. LV Family: CZ. Launch Vehicle: CZ-3. LV Configuration: Chang Zheng 3 CZ3-8 (26). FAILURE: Third stage failed to ignite. Partial Failure.. Failed Stage: 3.
  • Zhongxing-4 - . Payload: STTW 5. Mass: 1,025 kg (2,259 lb). Nation: China. Agency: Chinasat. Program: Chinasat. Class: Communications. Type: Military communications satellite. Spacecraft: DFH-2. USAF Sat Cat: 21833 . COSPAR: 1991-088A. Apogee: 34,041 km (21,152 mi). Perigee: 2,023 km (1,257 mi). Inclination: 32.3000 deg. Period: 632.60 min. Summary: Third stage failure; unusable orbit. DFH-2 operational communications satellite..

1994 November 29 - . 17:02 GMT - . Launch Site: Xichang. Launch Complex: Xichang LC2. LV Family: CZ. Launch Vehicle: CZ-3A. LV Configuration: Chang Zheng 3A CZ3A-2 (36).
  • Zhongxing-5 - . Mass: 2,230 kg (4,910 lb). Nation: China. Agency: Chinasat. Program: Chinasat. Class: Communications. Type: Military communications satellite. Spacecraft: DFH-3. Completed Operations Date: 1994-12-01 . USAF Sat Cat: 23415 . COSPAR: 1994-080A. Apogee: 35,957 km (22,342 mi). Perigee: 35,225 km (21,887 mi). Inclination: 0.1500 deg. Period: 1,426.15 min. The first test launch of a DFH-3 by a CZ-3A launch vehicle was successful in attaining the proper transfer orbit, but during the subsequent manoeuvres to achieve geostationary orbit, the DFH-3 failed due to a malfunction of the satellite on-board propulsion system. The satellite was positioned at 132 deg E prior to the failure. As of 4 September 2001 located at 113.80 deg E drifting at 2.499 deg E per day. As of 2007 Mar 2 located at 90.02E drifting at 2.513E degrees per day.

1996 August 18 - . 10:27 GMT - . Launch Site: Xichang. Launch Complex: Xichang LC1. LV Family: CZ. Launch Vehicle: CZ-3. LV Configuration: Chang Zheng 3 CZ3-11 (42).
  • Zhongxing 7 - . Payload: Zhongxing 7. Nation: China. Agency: Chinasat. Program: Chinasat. Class: Communications. Type: Military communications satellite. Spacecraft: HS 376. USAF Sat Cat: 24282 . COSPAR: 1996-048A. Apogee: 46,499 km (28,893 mi). Perigee: 21,674 km (13,467 mi). Inclination: 26.3000 deg. Period: 1,350.20 min.

1997 May 11 - . 16:17 GMT - . Launch Site: Xichang. Launch Complex: Xichang LC2. LV Family: CZ. Launch Vehicle: CZ-3A. LV Configuration: Chang Zheng 3A CZ3A-3 (44).
  • Zhongxing-6 - . Mass: 2,200 kg (4,800 lb). Nation: China. Agency: Chinasat. Program: Chinasat. Class: Communications. Type: Military communications satellite. Spacecraft: DFH-3. USAF Sat Cat: 24798 . COSPAR: 1997-021A. Apogee: 35,797 km (22,243 mi). Perigee: 35,776 km (22,230 mi). Inclination: 0.0000 deg. Period: 1,436.10 min. The telecommunications satellite, the most sophisticated and complex satellite ever built in China, was equipped with 24 transponders used for television, digital transmission and other telecommunications services. It had a design life eight years. After over one year of tests the satellite was delivered to the end user, China Telecommunications Broadcast Satellite Corporation (Chinasat) on August 12 1998. A long term operation contract for the redesignated Chinasat-6 was signed by the China Academy of Space Technology (CAST), Chinasat and the Xian Satellite Control Center. Chinasat-6 operated in geosynchronous orbit at 125 deg E in 1997-1999. As of 5 September 2001 located at 124.99 deg E drifting at 0.011 deg W per day. As of 2007 Mar 6 located at 123.93E drifting at 0.104W degrees per day.

2000 January 25 - . 16:45 GMT - . Launch Site: Xichang. Launch Complex: Xichang LC2. LV Family: CZ. Launch Vehicle: CZ-3A. LV Configuration: Chang Zheng 3A CZ3A-4 (60).
  • Zhongxing-22 - . Mass: 2,300 kg (5,000 lb). Nation: China. Agency: SISE. Manufacturer: CAST. Program: Chinasat. Class: Communications. Type: Military communications satellite. Spacecraft: FH-1. USAF Sat Cat: 26058 . COSPAR: 2000-003A. Apogee: 35,794 km (22,241 mi). Perigee: 35,781 km (22,233 mi). Inclination: 3.2000 deg. Period: 1,436.10 min. First Chinese military communications satellite. Perhaps an update of the DFH-3 design. Stationed at 98 deg E. The first in a planned constellation of satellites to be launched through 2010. Positioned in geosynchronous orbit at 98 deg E in 2000. As of 5 September 2001 located at 98.03 deg E drifting at 0.005 deg W per day. As of 2007 Mar 10 located at 97.95E drifting at 0.009W degrees per day.

2003 November 14 - . 16:01 GMT - . Launch Site: Xichang. Launch Complex: Xichang LC2. LV Family: CZ. Launch Vehicle: CZ-3A. LV Configuration: Chang Zheng 3A CZ3A-8 (74).
  • Zhongxing 20 - . Payload: Feng Huo 2. Mass: 2,300 kg (5,000 lb). Nation: China. Agency: SISE. Program: Chinasat. Class: Communications. Type: Military communications satellite. Spacecraft: DFH-3. USAF Sat Cat: 28082 . COSPAR: 2003-052A. Apogee: 35,811 km (22,251 mi). Perigee: 35,762 km (22,221 mi). Inclination: 0.0000 deg. Period: 1,436.10 min. Summary: Military communications satellite. As of 2007 Mar 11 located at 103.00E drifting at 0.010W degrees per day..

2006 September 12 - . 16:02 GMT - . Launch Site: Xichang. Launch Complex: Xichang LC2. LV Family: CZ. Launch Vehicle: CZ-3A. LV Configuration: Chang Zheng 3A CZ3A-10 (91).
  • Zhongxing 22A - . Mass: 2,300 kg (5,000 lb). Nation: China. Agency: CTBSC. Manufacturer: CAST. Program: Chinasat. Class: Communications. Type: Military communications satellite. Spacecraft: FH-1. USAF Sat Cat: 29398 . COSPAR: 2006-038A. Apogee: 35,817 km (22,255 mi). Perigee: 35,757 km (22,218 mi). Inclination: 0.4000 deg. Period: 1,000.00 min. Summary: Military communications satellite, launched to replace Zhongxing 22 in geosynchronous orbit at 98.0 E. As of 2007 Mar 10 located at 98.10E drifting at 0.006W degrees per day..

2007 July 5 - . 12:08 GMT - . Launch Site: Xichang. Launch Complex: Xichang LC2. LV Family: CZ. Launch Vehicle: CZ-3B. LV Configuration: Chang Zheng 3B CZ3B (101).
  • Chinasat 6B - . Payload: Spacebus 4000C2. Mass: 4,600 kg (10,100 lb). Nation: China. Agency: ChinaSatCom. Manufacturer: Alenia. Program: Chinasat. Class: Communications. Type: Civilian communications satellite. Spacecraft: Spacebus 4000. USAF Sat Cat: 31800 . COSPAR: 2007-031A. Apogee: 35,797 km (22,243 mi). Perigee: 35,775 km (22,229 mi). Inclination: 0.0200 deg. Period: 1,436.07 min. Summary: Direct broadcast satellite, capable of transmitting 300 television channels using 38 transponders. To be positioned at 115.5 deg E, beaming signals to China, Southeast Asia, and Oceania. Planned mission life 15 years..

2008 June 9 - . 12:15 GMT - . Launch Site: Xichang. LV Family: CZ. Launch Vehicle: CZ-3B.
  • Zhongxing 9 - . Nation: China. Agency: SISE. Program: Chinasat. Class: Communications. Type: Military communications satellite. Spacecraft: Spacebus 4000. USAF Sat Cat: 33051 . COSPAR: 2008-028A. Apogee: 35,804 km (22,247 mi). Perigee: 35,770 km (22,220 mi). Inclination: 0.0000 deg. Period: 1,436.10 min. Summary: Launched to support Olympic games; 22 J-band transponders; positioned at 92.2 deg E..

2010 September 4 - . 16:14 GMT - . Launch Site: Xichang. LV Family: CZ. Launch Vehicle: CZ-3B.
  • Chinasat 6A - . Payload: Zhongxing 6A. Mass: 5,100 kg (11,200 lb). Nation: China. Agency: SISE. Program: Chinasat. Class: Communications. Type: Communications satellite. Spacecraft: DFH-4. USAF Sat Cat: 37150 . COSPAR: 2010-042A. Apogee: 35,795 km (22,241 mi). Perigee: 35,778 km (22,231 mi). Inclination: 0.1000 deg. Period: 1,436.10 min. Summary: C and Ku band communications transponders..

2010 November 24 - . 16:09 GMT - . Launch Site: Xichang. LV Family: CZ. Launch Vehicle: CZ-3A.
  • Chinasat 20A - . Payload: Zhongxing 20A. Nation: China. Program: Chinasat. Class: Communications. Type: Communications satellite. Spacecraft: DFH-3. USAF Sat Cat: 37234 . COSPAR: 2010-064A. Apogee: 35,795 km (22,241 mi). Perigee: 35,778 km (22,231 mi). Inclination: 0.4000 deg. Period: 1,436.10 min.

2011 June 20 - . 16:13 GMT - . Launch Site: Xichang. LV Family: CZ. Launch Vehicle: CZ-3B. LV Configuration: CZ-3B(E).
  • Zhongxing-10 - . Payload: Chinasat 10. Mass: 5,000 kg (11,000 lb). Nation: China. Program: Chinasat. Class: Communications. Type: Communications satellite. Spacecraft: DFH-4. USAF Sat Cat: 37677 . COSPAR: 2011-026A. Apogee: 35,812 km (22,252 mi). Perigee: 35,764 km (22,222 mi). Inclination: 0.0000 deg. Period: 1,436.20 min. Summary: Chinese communications satellite, stationed over 103.5 deg E. AKA ChinaSat 10, Xinnuo-5, and Sinosat-5..

2011 September 17 - . 16:33 GMT - . Launch Site: Xichang. LV Family: CZ. Launch Vehicle: CZ-3B.
  • Chinasat 1A - . Nation: China. Program: Chinasat. Class: Communications. Type: Communications satellite. Spacecraft: DFH-4. USAF Sat Cat: 37804 . COSPAR: 2011-047A. Apogee: 35,794 km (22,241 mi). Perigee: 35,781 km (22,233 mi). Inclination: 0.5000 deg. Period: 1,436.10 min. Summary: Military communications satellite..

Home - Browse - Contact
© / Conditions for Use