CZ-3B R/B
Satellite information CZ-3B R/B
| Spacetrack Directory Name | CZ-3B R/B |
| Orbit launches |
2026-06-16 |
| Deorbitation |
|
| Country/organisation of origin | Chiny (PRC) |
| Starting point | XSC |
| Perigee | 117 km |
| Apogee | 36501 km |
Additional information CZ-3B R/B
CZ-3B R/B, 69571 is space debris in HEO originally from a launch on Tue, 16 Jun 2026 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 16.06.2026y. Inclination CZ-3B R/B satellite 63.18°.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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