FENGYUN 2A DEB
Satellite information FENGYUN 2A DEB
| Spacetrack Directory Name | FENGYUN 2A DEB |
| Follow FENGYUN 2A DEB | FENGYUN 2A DEB Tracker |
| Pass predictions FENGYUN 2A DEB | Pass predictions FENGYUN 2A DEB |
| Orbit launches |
1997-06-10 (29 years ago)
|
| Days in orbit | 10687 |
| Country/organisation of origin | Chiny (PRC) |
| Starting point | XICLF (Xichang Launch Facility, China) |
| Perigee | 35449 km |
| Apogee | 36142 km |
| Orbit slope (inclination) | 14.85° |
| Laps per day | 1 |
| Height FENGYUN 2A DEB | 35787.71 km |
Additional information FENGYUN 2A DEB
FENGYUN 2A DEB, 43355 is space debris in GEO originally from a launch on Tue, 10 Jun 1997 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 2A DEB Date of exalting 10.06.1997y. Average height of ISS FENGYUN 2A DEB hundred 35787.71 km. Average velocity FENGYUN 2A DEB is 11068.94 km/h. Inclination FENGYUN 2A DEB satellite 14.85°.TLE
Average velocity FENGYUN 2A DEB
Average inclination FENGYUN 2A DEB
Mean right ascension of the ascending node (RAAN) FENGYUN 2A DEB
Mean argument of perigee FENGYUN 2A DEB
Mean semi-major axis of the orbit FENGYUN 2A DEB
Mean orbital eccentricity FENGYUN 2A DEB
ISS
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