CZ-8A R/B
Satellite information CZ-8A R/B
| Spacetrack Directory Name | CZ-8A R/B |
| Follow CZ-8A R/B | CZ-8A R/B Tracker |
| Pass predictions CZ-8A R/B | Pass predictions CZ-8A R/B |
| Orbit launches |
2025-12-06 (8 months ago)
|
| Days in orbit | 258 |
| Country/organisation of origin | Chiny (PRC) |
| Starting point | WSC (Wenchang Spacecraft Launch Site) |
| Perigee | 705 km |
| Apogee | 875 km |
| Orbit slope (inclination) | 50.01° |
| Laps per day | 14 |
| Height CZ-8A R/B | 796.28 km |
Additional information CZ-8A R/B
CZ-8A R/B, 66924 is space debris in LEO originally from a launch on Sat, 06 Dec 2025 UTC launched from the Wenchang Satellite Launch Center (WSC). 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-8A R/B Date of exalting 06.12.2025y. Average height of ISS CZ-8A R/B hundred 796.28 km. Average velocity CZ-8A R/B is 26846.99 km/h. Inclination CZ-8A R/B satellite 50.01°.TLE
Average velocity CZ-8A R/B
Average inclination CZ-8A R/B
Mean right ascension of the ascending node (RAAN) CZ-8A R/B
Mean argument of perigee CZ-8A R/B
Mean semi-major axis of the orbit CZ-8A R/B
Mean orbital eccentricity CZ-8A R/B
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