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Beidou-GEO

China

Original archive entry. The text, images and links below are kept as they were written.

Beidou G5
Beidou G5
Credit: Manufacturer Image

The Beidou-2 GEO (geosynchronous orbit) satellites incorporated Beidou-1 location and messaging technology for backward compatibility with existing receivers. Five of these were operational as of the end of 2010.

Country
China
Launch Vehicles
Chang Zheng 3C
Bibliography
12151, 12152

Chronology

7 events

2009 April 14

16:16 GMT - . Launch Site: Xichang. LV Family: CZ. Launch Vehicle: Chang Zheng 3C.
  • Beidou G2 - . Payload: Beidou DW2. Mass: 3,800 kg (8,300 lb). Nation: China. Agency: SISE. Class: Navigation. Type: Navigation satellite. Spacecraft: Beidou-GEO. USAF Sat Cat: 34779 . COSPAR: 2009-018A. Apogee: 35,799 km (22,244 mi). Perigee: 35,783 km (22,234 mi). Inclination: 0.70 deg. Period: 1,436.30 min. First launch of the geostationary component of the Beidou-2 navigation satellite constellation. Experienced control problems; as of 2010 not in the operational constellation..

2010 January 16

16:12 GMT - . Launch Site: Xichang. LV Family: CZ. Launch Vehicle: Chang Zheng 3C.
  • Beidou G1 - . Payload: Beidou DW3. Mass: 3,800 kg (8,300 lb). Nation: China. Agency: SISE. Class: Navigation. Type: Navigation satellite. Spacecraft: Beidou-GEO. USAF Sat Cat: 36287 . COSPAR: 2010-001A. Apogee: 35,972 km (22,351 mi). Perigee: 35,600 km (22,100 mi). Inclination: 1.80 deg. Period: 1,436.10 min. First successful launch in the geostationary component of the Beidou-2 navigation satellite constellation. Stationed at 144.5 deg E..

2010 June 2

15:53 GMT - . Launch Site: Xichang. LV Family: CZ. Launch Vehicle: Chang Zheng 3C.
  • Beidou G3 - . Payload: Beidou DW4. Mass: 3,800 kg (8,300 lb). Nation: China. Agency: SISE. Class: Navigation. Type: Navigation satellite. Spacecraft: Beidou-GEO. USAF Sat Cat: 36590 . COSPAR: 2010-024A. Apogee: 35,796 km (22,242 mi). Perigee: 35,776 km (22,230 mi). Inclination: 1.80 deg. Period: 1,436.00 min. Second successful launch in the geostationary component of the Beidou-2 navigation satellite constellation. Stationed at 84 deg E..

2010 October 31

16:26 GMT - . Launch Site: Xichang. LV Family: CZ. Launch Vehicle: Chang Zheng 3C.
  • Beidou G4 - . Payload: Beidou DW6. Mass: 3,800 kg (8,300 lb). Nation: China. Agency: SISE. Class: Navigation. Type: Navigation satellite. Spacecraft: Beidou-GEO. USAF Sat Cat: 37210 . COSPAR: 2010-057A. Apogee: 35,793 km (22,240 mi). Perigee: 35,781 km (22,233 mi). Inclination: 1.60 deg. Period: 1,436.10 min. Third successful launch in the geostationary component of the Beidou-2 navigation satellite constellation. Stationed at 160 deg E. These three launches in one year completed that portion of the constellation..

2012 February 24

16:12 GMT - . Launch Site: Xichang. LV Family: CZ. Launch Vehicle: Chang Zheng 3C.
  • Beidou G5 - . Payload: Beidou DW 11. Mass: 3,800 kg (8,300 lb). Nation: China. Class: Navigation. Type: Navigation satellite. Spacecraft: Beidou-GEO. USAF Sat Cat: 38091 . COSPAR: 2012-008A. Apogee: 35,790 km (22,230 mi). Perigee: 35,784 km (22,235 mi). Inclination: 1.70 deg. Period: 1,436.10 min. Stationed in geostationary orbit at 58.7 deg E..

2012 October 25

15:33 GMT - . Launch Site: Xichang. LV Family: CZ. Launch Vehicle: Chang Zheng 3C.
  • Beidou G6 - . Payload: Beidou DW16. Mass: 3,800 kg (8,300 lb). Nation: China. Class: Navigation. Type: Navigation satellite. Spacecraft: Beidou-GEO. USAF Sat Cat: 38953 . COSPAR: 2012-059A. Apogee: 35,797 km (22,243 mi). Perigee: 35,776 km (22,230 mi). Inclination: 1.80 deg. Period: 1,436.10 min. Reached geostationary orbital station at 80.4 E on 1 November. The transfer orbit had an unusually low perigee of around 160 km. Stationed at 80 deg E..

2016 June 12

15:30 GMT - . Launch Site: Xichang. Launch Complex: Xichang LC3. LV Family: CZ. Launch Vehicle: Chang Zheng 3C.
  • Beidou DW 23 - . Payload: Beidou G7. Nation: China. Class: Navigation. Type: Navigation satellite. Spacecraft: Beidou-GEO. USAF Sat Cat: 41586 . COSPAR: 2016-037A. Apogee: 34,574 km (21,483 mi). Perigee: 217 km (134 mi). Inclination: 19.30 deg. 7th geostationary satellite in the Beidou-2 generation..