CZ-6A DEB
Satellite information CZ-6A DEB - Satelita
| Spacetrack Directory Name | CZ-6A DEB |
| Alternative name | Satelita |
| Follow CZ-6A DEB | CZ-6A DEB Tracker |
| Pass predictions CZ-6A DEB | Pass predictions CZ-6A DEB |
| Country/organisation of origin | Chiny (PRC) |
| Starting point | |
| Perigee | 787 km |
| Apogee | 862 km |
| Orbit slope (inclination) | 98.83° |
| Laps per day | 14 |
| Height CZ-6A DEB | 835.5 km |
Additional information CZ-6A DEB
CZ-6A DEB, 66789 is space debris in SSO originally from a Chinese launch on Fri, 11 Nov 2022 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.
Average height of ISS CZ-6A DEB hundred 835.5 km. Average velocity CZ-6A DEB is 26771.97 km/h. Inclination CZ-6A DEB satellite 98.83°.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
ISS
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