FENGYUN 2C AKM
Satellite information FENGYUN 2C AKM
| Spacetrack Directory Name | FENGYUN 2C AKM |
| Follow FENGYUN 2C AKM | FENGYUN 2C AKM Tracker |
| Pass predictions FENGYUN 2C AKM | Pass predictions FENGYUN 2C AKM |
| Orbit launches |
2004-10-19 (21 years ago)
|
| Days in orbit | 7989 |
| Country/organisation of origin | Chiny (PRC) |
| Starting point | XICLF (Xichang Launch Facility, China) |
| Perigee | 35391 km |
| Apogee | 35591 km |
| Orbit slope (inclination) | 12.59° |
| Laps per day | 1 |
| Height FENGYUN 2C AKM | 35491.28 km |
Additional information FENGYUN 2C AKM
FENGYUN 2C AKM, 28491 is space debris in GEO originally from a launch on Tue, 19 Oct 2004 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 2C AKM Date of exalting 19.10.2004y. Average height of ISS FENGYUN 2C AKM hundred 35491.28 km. Average velocity FENGYUN 2C AKM is 11107.84 km/h. Inclination FENGYUN 2C AKM satellite 12.58°.TLE
Average velocity FENGYUN 2C AKM
Average inclination FENGYUN 2C AKM
Mean right ascension of the ascending node (RAAN) FENGYUN 2C AKM
Mean argument of perigee FENGYUN 2C AKM
Mean semi-major axis of the orbit FENGYUN 2C AKM
Mean orbital eccentricity FENGYUN 2C AKM
ISS
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