CZ-3B R/B
Satellite information CZ-3B R/B
| Spacetrack Directory Name | CZ-3B R/B |
| Orbit launches |
2025-03-26 |
| Deorbitation |
|
| Country/organisation of origin | Chiny (PRC) |
| Starting point | XICLF (Xichang Launch Facility, China) |
| Perigee | 169 km |
| Apogee | 34661 km |
| Height CZ-3B R/B | 17494.72 km |
Additional information CZ-3B R/B
CZ-3B R/B, 63362 is space debris in HEO originally from a launch on Wed, 26 Mar 2025 UTC launched from the Xichang Space Center, China (XSC). 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-3B R/B Date of exalting 26.03.2025y. Average height of ISS CZ-3B R/B hundred 17494.72 km. Average velocity CZ-3B R/B is 14271.93 km/h. Inclination CZ-3B R/B satellite 26.84°.Average velocity CZ-3B R/B
Average inclination CZ-3B R/B
Mean right ascension of the ascending node (RAAN) CZ-3B R/B
Mean argument of perigee CZ-3B R/B
Mean semi-major axis of the orbit CZ-3B R/B
Mean orbital eccentricity CZ-3B R/B
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