FENGYUN 2E AKM
Satellite information FENGYUN 2E AKM
| Spacetrack Directory Name | FENGYUN 2E AKM |
| Follow FENGYUN 2E AKM | FENGYUN 2E AKM Tracker |
| Pass predictions FENGYUN 2E AKM | Pass predictions FENGYUN 2E AKM |
| 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 |
| Perigee | 35133 km |
| Apogee | 35432 km |
| Orbit slope (inclination) | 9.99° |
| Laps per day | 1 |
| Height FENGYUN 2E AKM | 35283.99 km |
Additional information FENGYUN 2E AKM
FENGYUN 2E AKM, 33465 is space debris in GEO originally from a launch on Tue, 23 Dec 2008 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 2E AKM Date of exalting 23.12.2008y. Average height of ISS FENGYUN 2E AKM hundred 35283.99 km. Average velocity FENGYUN 2E AKM is 11135.38 km/h. Inclination FENGYUN 2E AKM satellite 9.97°.TLE
Average velocity FENGYUN 2E AKM
Average inclination FENGYUN 2E AKM
Mean right ascension of the ascending node (RAAN) FENGYUN 2E AKM
Mean argument of perigee FENGYUN 2E AKM
Mean semi-major axis of the orbit FENGYUN 2E AKM
Mean orbital eccentricity FENGYUN 2E AKM
ISS
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