FENGYUN 2F AKM
Satellite information FENGYUN 2F AKM
| Spacetrack Directory Name | FENGYUN 2F AKM |
| Follow FENGYUN 2F AKM | FENGYUN 2F AKM Tracker |
| Pass predictions FENGYUN 2F AKM | Pass predictions FENGYUN 2F AKM |
| Orbit launches |
2012-01-13 (14 years ago)
|
| Days in orbit | 5410 |
| Country/organisation of origin | Chiny (PRC) |
| Starting point | XICLF (Xichang Launch Facility, China) |
| Perigee | 35787 km |
| Apogee | 36281 km |
| Orbit slope (inclination) | 9.49° |
| Laps per day | 1 |
| Height FENGYUN 2F AKM | 36033.68 km |
Additional information FENGYUN 2F AKM
FENGYUN 2F AKM, 38072 is space debris in GEO originally from a launch on Fri, 13 Jan 2012 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 2F AKM Date of exalting 13.01.2012y. Average height of ISS FENGYUN 2F AKM hundred 36033.68 km. Average velocity FENGYUN 2F AKM is 11036.75 km/h. Inclination FENGYUN 2F AKM satellite 9.39°.TLE
Average velocity FENGYUN 2F AKM
Average inclination FENGYUN 2F AKM
Mean right ascension of the ascending node (RAAN) FENGYUN 2F AKM
Mean argument of perigee FENGYUN 2F AKM
Mean semi-major axis of the orbit FENGYUN 2F AKM
Mean orbital eccentricity FENGYUN 2F AKM
ISS
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