CZ-6A DEB
Satellite information CZ-6A DEB
| Spacetrack Directory Name | CZ-6A DEB |
| Follow CZ-6A DEB | CZ-6A DEB Tracker |
| Pass predictions CZ-6A DEB | Pass predictions CZ-6A DEB |
| Orbit launches |
2025-05-11 (one year ago)
|
| Days in orbit | 469 |
| Country/organisation of origin | Chiny (PRC) |
| Starting point | TAISC (Taiyuan Space Center, China) |
| Perigee | 794 km |
| Apogee | 810 km |
| Orbit slope (inclination) | 86° |
| Laps per day | 14 |
| Height CZ-6A DEB | 812.92 km |
Additional information CZ-6A DEB
CZ-6A DEB, 63923 is space debris in LEO originally from a launch on Sun, 11 May 2025 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 CZ-6A DEB Date of exalting 11.05.2025y. Average height of ISS CZ-6A DEB hundred 812.92 km. Average velocity CZ-6A DEB is 26813.88 km/h. Inclination CZ-6A DEB satellite 86°.TLE
Average velocity CZ-6A DEB
Average inclination CZ-6A DEB
Mean right ascension of the ascending node (RAAN) CZ-6A DEB
Mean argument of perigee CZ-6A DEB
Mean semi-major axis of the orbit CZ-6A DEB
Mean orbital eccentricity CZ-6A DEB
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