FENGYUN 2A
Satellite information FENGYUN 2A - FY-2A
| Spacetrack Directory Name | FENGYUN 2A |
| Alternative name | FY-2A |
| Follow FENGYUN 2A | FENGYUN 2A Tracker |
| Pass predictions FENGYUN 2A | Pass predictions FENGYUN 2A |
| Orbit launches |
1997-06-10 (29 years ago)
|
| Days in orbit | 10688 |
| Country/organisation of origin | Chiny (PRC) |
| Starting point | XICLF (Xichang Launch Facility, China) |
| Perigee | 36593 km |
| Apogee | 37433 km |
| Orbit slope (inclination) | 15.7° |
| Laps per day | 1 |
| Height FENGYUN 2A | 37016.54 km |
Additional information FENGYUN 2A
FENGYUN 2A, 24834 is a payload satellite owned by CNMSC (CN) in GEO that was launched on Tue, 10 Jun 1997 UTC via a CHANG ZHENG 3 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 2A Date of exalting 10.06.1997y. Average height of ISS FENGYUN 2A hundred 37016.54 km. Average velocity FENGYUN 2A is 10910.87 km/h. Inclination FENGYUN 2A satellite 15.69°.TLE
Average velocity FENGYUN 2A
Average inclination FENGYUN 2A
Mean right ascension of the ascending node (RAAN) FENGYUN 2A
Mean argument of perigee FENGYUN 2A
Mean semi-major axis of the orbit FENGYUN 2A
Mean orbital eccentricity FENGYUN 2A
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