FENGYUN 2E
Satellite information FENGYUN 2E - FY-2E
| Spacetrack Directory Name | FENGYUN 2E |
| Alternative name | FY-2E |
| Follow FENGYUN 2E | FENGYUN 2E Tracker |
| Pass predictions FENGYUN 2E | Pass predictions FENGYUN 2E |
| Orbit launches |
2008-12-23 (17 years ago)
|
| Days in orbit | 6460 |
| Country/organisation of origin | Chiny (PRC) |
| Starting point | XICLF (Xichang Launch Facility, China) |
| WWW | Here |
| Categories | |
| Perigee | 35769 km |
| Apogee | 35800 km |
| Orbit slope (inclination) | 9.43° |
| Laps per day | 1 |
| Orbit | GEO |
| Height FENGYUN 2E | 36111.6 km |
Additional information FENGYUN 2E
FENGYUN 2E, 33463 is a payload satellite owned by CNMSC (CN) in GEO that was launched on Tue, 23 Dec 2008 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 FENGYUN 2E Date of exalting 23.12.2008y. Average height of ISS FENGYUN 2E hundred 36111.6 km. Average velocity FENGYUN 2E is 11026.53 km/h. Inclination FENGYUN 2E satellite 9.41°.TLE
Average velocity FENGYUN 2E
Average inclination FENGYUN 2E
Mean right ascension of the ascending node (RAAN) FENGYUN 2E
Mean argument of perigee FENGYUN 2E
Mean semi-major axis of the orbit FENGYUN 2E
Mean orbital eccentricity FENGYUN 2E
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