YAOGAN 25C DEB
Satellite information YAOGAN 25C DEB
| Spacetrack Directory Name | YAOGAN 25C DEB |
| Follow YAOGAN 25C DEB | YAOGAN 25C DEB Tracker |
| Pass predictions YAOGAN 25C DEB | Pass predictions YAOGAN 25C DEB |
| Orbit launches |
2014-12-10 (11 years ago)
|
| Days in orbit | 4347 |
| Country/organisation of origin | Chiny (PRC) |
| Starting point | JSC (Jiuquan Satellite Launch Center, China) |
| Perigee | 742 km |
| Apogee | 1226 km |
| Orbit slope (inclination) | 63.37° |
| Laps per day | 14 |
| Height YAOGAN 25C DEB | 982.52 km |
Additional information YAOGAN 25C DEB
YAOGAN 25C DEB, 69732 is space debris in LEO originally from a Commonwealth of Independent States-origin launch on Wed, 10 Dec 2014 UTC launched from the Jiuquan Satellite Launch Center, China (JSC). 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 YAOGAN 25C DEB Date of exalting 10.12.2014y. Average height of ISS YAOGAN 25C DEB hundred 982.52 km. Average velocity YAOGAN 25C DEB is 26504.46 km/h. Inclination YAOGAN 25C DEB satellite 63.37°.TLE
Average velocity YAOGAN 25C DEB
Average inclination YAOGAN 25C DEB
Mean right ascension of the ascending node (RAAN) YAOGAN 25C DEB
Mean argument of perigee YAOGAN 25C DEB
Mean semi-major axis of the orbit YAOGAN 25C DEB
Mean orbital eccentricity YAOGAN 25C DEB
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