FENGYUN 4A
Satellite information FENGYUN 4A
| Spacetrack Directory Name | FENGYUN 4A |
| Follow FENGYUN 4A | FENGYUN 4A Tracker |
| Pass predictions FENGYUN 4A | Pass predictions FENGYUN 4A |
| Orbit launches |
2016-12-10 (9 years ago)
|
| Days in orbit | 3618 |
| Country/organisation of origin | Chiny (PRC) |
| Starting point | XICLF (Xichang Launch Facility, China) |
| Categories | |
| Perigee | 35764 km |
| Apogee | 35807 km |
| Orbit slope (inclination) | 2.67° |
| Laps per day | 1 |
| Orbit | GEO |
| Height FENGYUN 4A | 35786.42 km |
Additional information FENGYUN 4A
FENGYUN 4A, 41882 is a payload satellite owned by CNMSC (CN) in GEO that was launched on Sat, 10 Dec 2016 UTC via a CHANG ZHENG 3B 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 FENGYUN 4A Date of exalting 10.12.2016y. Average height of ISS FENGYUN 4A hundred 35786.42 km. Average velocity FENGYUN 4A is 11068.94 km/h. Inclination FENGYUN 4A satellite 2.21°.TLE
Average velocity FENGYUN 4A
Average inclination FENGYUN 4A
Mean right ascension of the ascending node (RAAN) FENGYUN 4A
Mean argument of perigee FENGYUN 4A
Mean semi-major axis of the orbit FENGYUN 4A
Mean orbital eccentricity FENGYUN 4A
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