CHINASAT 31 (BEIDOU 1B)
Satellite information CHINASAT 31 (BEIDOU 1B) - CHINASAT-31
| Spacetrack Directory Name | CHINASAT 31 (BEIDOU 1B) |
| Alternative name | CHINASAT-31 |
| Follow CHINASAT 31 (BEIDOU 1B) | CHINASAT 31 (BEIDOU 1B) Tracker |
| Pass predictions CHINASAT 31 (BEIDOU 1B) | Pass predictions CHINASAT 31 (BEIDOU 1B) |
| Orbit launches |
2000-12-20 (25 years ago)
|
| Days in orbit | 9389 |
| Country/organisation of origin | Chiny (PRC) |
| Starting point | XICLF (Xichang Launch Facility, China) |
| WWW | Here |
| Perigee | 35721 km |
| Apogee | 36427 km |
| Orbit slope (inclination) | 12.7° |
| Laps per day | 1 |
| Height CHINASAT 31 (BEIDOU 1B) | 36076.8 km |
Additional information CHINASAT 31 (BEIDOU 1B)
CHINASAT 31 (BEIDOU 1B), 26643 is a payload satellite owned by CNSA (CN) in GEO that was launched on Wed, 20 Dec 2000 UTC via a CHANG ZHENG 3A launch vehicle from the Xichang Space Center, China (XSC). Payloads include a variety of satellites, spacecraft, and rockets equipped with specific instruments for various scientific and technological missions. These include communications satellites like Starlink; space stations such as the ISS; scientific satellites like the Hubble; Earth observation satellites from companies like Planet Labs, Umbra, and HawkEye 360; GPS; miniature CubeSats for education and research; and military/defense satellites.
satellite CHINASAT 31 (BEIDOU 1B) Date of exalting 20.12.2000y. Average height of ISS CHINASAT 31 (BEIDOU 1B) hundred 36076.8 km. Average velocity CHINASAT 31 (BEIDOU 1B) is 11031.03 km/h. Inclination CHINASAT 31 (BEIDOU 1B) satellite 12.69°.TLE
Average orbit height CHINASAT 31 (BEIDOU 1B)
Average velocity CHINASAT 31 (BEIDOU 1B)
Average inclination CHINASAT 31 (BEIDOU 1B)
Mean right ascension of the ascending node (RAAN) CHINASAT 31 (BEIDOU 1B)
Mean argument of perigee CHINASAT 31 (BEIDOU 1B)
Mean semi-major axis of the orbit CHINASAT 31 (BEIDOU 1B)
Mean orbital eccentricity CHINASAT 31 (BEIDOU 1B)
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