FENGYUN 2A AKM
Satellite information FENGYUN 2A AKM
| Spacetrack Directory Name | FENGYUN 2A AKM |
| Follow FENGYUN 2A AKM | FENGYUN 2A AKM Tracker |
| Pass predictions FENGYUN 2A AKM | Pass predictions FENGYUN 2A AKM |
| 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 | 34145 km |
| Apogee | 35997 km |
| Orbit slope (inclination) | 13.84° |
| Laps per day | 1 |
| Height FENGYUN 2A AKM | 35079.74 km |
Additional information FENGYUN 2A AKM
FENGYUN 2A AKM, 25611 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 AKM Date of exalting 10.06.1997y. Average height of ISS FENGYUN 2A AKM hundred 35079.74 km. Average velocity FENGYUN 2A AKM is 11163.24 km/h. Inclination FENGYUN 2A AKM satellite 13.84°.TLE
Average velocity FENGYUN 2A AKM
Average inclination FENGYUN 2A AKM
Mean right ascension of the ascending node (RAAN) FENGYUN 2A AKM
Mean argument of perigee FENGYUN 2A AKM
Mean semi-major axis of the orbit FENGYUN 2A AKM
Mean orbital eccentricity FENGYUN 2A AKM
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