FENGYUN 2G DEB
Satellite information FENGYUN 2G DEB
| Spacetrack Directory Name | FENGYUN 2G DEB |
| Follow FENGYUN 2G DEB | FENGYUN 2G DEB Tracker |
| Pass predictions FENGYUN 2G DEB | Pass predictions FENGYUN 2G DEB |
| Orbit launches |
2014-12-31 (11 years ago)
|
| Days in orbit | 4328 |
| Country/organisation of origin | Chiny (PRC) |
| Starting point | XICLF (Xichang Launch Facility, China) |
| WWW | Here |
| Perigee | 35126 km |
| Apogee | 36415 km |
| Orbit slope (inclination) | 7.84° |
| Laps per day | 1 |
| Height FENGYUN 2G DEB | 35797.38 km |
Additional information FENGYUN 2G DEB
FENGYUN 2G DEB, 43646 is space debris in GEO originally from a launch on Wed, 31 Dec 2014 UTC launched from the Xichang Space Center, China (XSC). Debris objects in space refer to the collection of defunct objects orbiting the Earth. Examples of debris include non-operational satellites, rocket bodies, and fragments generated from explosions, collisions, or faulty payload assembly.
satellite FENGYUN 2G DEB Date of exalting 31.12.2014y. Average height of ISS FENGYUN 2G DEB hundred 35797.38 km. Average velocity FENGYUN 2G DEB is 11067.8 km/h. Inclination FENGYUN 2G DEB satellite 7.76°.TLE
Average velocity FENGYUN 2G DEB
Average inclination FENGYUN 2G DEB
Mean right ascension of the ascending node (RAAN) FENGYUN 2G DEB
Mean argument of perigee FENGYUN 2G DEB
Mean semi-major axis of the orbit FENGYUN 2G DEB
Mean orbital eccentricity FENGYUN 2G DEB
ISS
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