FENGYUN 2F DEB
Satellite information FENGYUN 2F DEB
| Spacetrack Directory Name | FENGYUN 2F DEB |
| Follow FENGYUN 2F DEB | FENGYUN 2F DEB Tracker |
| Pass predictions FENGYUN 2F DEB | Pass predictions FENGYUN 2F DEB |
| 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 | 35137 km |
| Apogee | 36436 km |
| Orbit slope (inclination) | 9.42° |
| Laps per day | 1 |
| Height FENGYUN 2F DEB | 35809.34 km |
Additional information FENGYUN 2F DEB
FENGYUN 2F DEB, 43396 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 DEB Date of exalting 13.01.2012y. Average height of ISS FENGYUN 2F DEB hundred 35809.34 km. Average velocity FENGYUN 2F DEB is 11066.09 km/h. Inclination FENGYUN 2F DEB satellite 9.32°.TLE
Average velocity FENGYUN 2F DEB
Average inclination FENGYUN 2F DEB
Mean right ascension of the ascending node (RAAN) FENGYUN 2F DEB
Mean argument of perigee FENGYUN 2F DEB
Mean semi-major axis of the orbit FENGYUN 2F DEB
Mean orbital eccentricity FENGYUN 2F DEB
ISS
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