YAOGAN-50 02 DEB
Satellite information YAOGAN-50 02 DEB
| Spacetrack Directory Name | YAOGAN-50 02 DEB |
| Follow YAOGAN-50 02 DEB | YAOGAN-50 02 DEB Tracker |
| Pass predictions YAOGAN-50 02 DEB | Pass predictions YAOGAN-50 02 DEB |
| Orbit launches |
2026-03-15 (5 months ago)
|
| Days in orbit | 175 |
| Country/organisation of origin | Chiny (PRC) |
| Starting point | TSC |
| Perigee | 890 km |
| Apogee | 999 km |
| Orbit slope (inclination) | 142° |
| Laps per day | 14 |
| Height YAOGAN-50 02 DEB | 947.34 km |
Additional information YAOGAN-50 02 DEB
YAOGAN-50 02 DEB, 100564 is space debris in LEO originally from a Chinese launch on Sun, 15 Mar 2026 UTC launched from the Taiyaun Space Center, China (TSC). 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-50 02 DEB Date of exalting 15.03.2026y. Average height of ISS YAOGAN-50 02 DEB hundred 947.34 km. Average velocity YAOGAN-50 02 DEB is 26569.74 km/h. Inclination YAOGAN-50 02 DEB satellite 142°.TLE
Average velocity YAOGAN-50 02 DEB
Average inclination YAOGAN-50 02 DEB
Mean right ascension of the ascending node (RAAN) YAOGAN-50 02 DEB
Mean argument of perigee YAOGAN-50 02 DEB
Mean semi-major axis of the orbit YAOGAN-50 02 DEB
Mean orbital eccentricity YAOGAN-50 02 DEB
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