CHINASAT 20A
Satellite information CHINASAT 20A - CHINASAT-20A
| Spacetrack Directory Name | CHINASAT 20A |
| Alternative name | CHINASAT-20A |
| Follow CHINASAT 20A | CHINASAT 20A Tracker |
| Pass predictions CHINASAT 20A | Pass predictions CHINASAT 20A |
| Orbit launches |
2010-11-24 (15 years ago)
|
| Days in orbit | 5757 |
| Country/organisation of origin | Chiny (PRC) |
| Starting point | XICLF (Xichang Launch Facility, China) |
| Categories | |
| Perigee | 35776 km |
| Apogee | 35794 km |
| Orbit slope (inclination) | 7.46° |
| Laps per day | 1 |
| Orbit | GEO |
| Height CHINASAT 20A | 36313.31 km |
Additional information CHINASAT 20A
CHINASAT 20A, 37234 is a payload satellite owned by PLA GAD (CN) in GEO that was launched on Wed, 24 Nov 2010 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 20A Date of exalting 24.11.2010y. Average height of ISS CHINASAT 20A hundred 36313.31 km. Average velocity CHINASAT 20A is 11000.54 km/h. Inclination CHINASAT 20A satellite 7.44°.TLE
Average velocity CHINASAT 20A
Average inclination CHINASAT 20A
Mean right ascension of the ascending node (RAAN) CHINASAT 20A
Mean argument of perigee CHINASAT 20A
Mean semi-major axis of the orbit CHINASAT 20A
Mean orbital eccentricity CHINASAT 20A
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