CZ-6A DEB
Satellite information CZ-6A DEB - YAOGAN-40 01C
| Spacetrack Directory Name | CZ-6A DEB |
| Alternative name | YAOGAN-40 01C |
| Follow CZ-6A DEB | CZ-6A DEB Tracker |
| Pass predictions CZ-6A DEB | Pass predictions CZ-6A DEB |
| Orbit launches |
2023-09-10 (2 years ago)
|
| Days in orbit | 1084 |
| Country/organisation of origin | Chiny (PRC) |
| Starting point | TAISC (Taiyuan Space Center, China) |
| Perigee | 795 km |
| Apogee | 809 km |
| Orbit slope (inclination) | 85.99° |
| Laps per day | 14 |
| Height CZ-6A DEB | 809.14 km |
Additional information CZ-6A DEB
CZ-6A DEB, 57834 is space debris in LEO originally from a launch on Sun, 10 Sep 2023 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 10.09.2023y. Average height of ISS CZ-6A DEB hundred 809.14 km. Average velocity CZ-6A DEB is 26820.96 km/h. Inclination CZ-6A DEB satellite 85.99°.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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