CZ-3B R/B
Satellite information CZ-3B R/B
| Spacetrack Directory Name | CZ-3B R/B |
| Follow CZ-3B R/B | CZ-3B R/B Tracker |
| Pass predictions CZ-3B R/B | Pass predictions CZ-3B R/B |
| Orbit launches |
2025-02-22 (one year ago)
|
| Days in orbit | 560 |
| Country/organisation of origin | Chiny (PRC) |
| Starting point | XICLF (Xichang Launch Facility, China) |
| Perigee | 197 km |
| Apogee | 35755 km |
| Orbit slope (inclination) | 27.23° |
| Laps per day | 3 |
| Height CZ-3B R/B | 19686.44 km |
Additional information CZ-3B R/B
CZ-3B R/B, 63076 is space debris in HEO originally from a launch on Sat, 22 Feb 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 22.02.2025y. Average height of ISS CZ-3B R/B hundred 19686.44 km. Average velocity CZ-3B R/B is 13610.89 km/h. Inclination CZ-3B R/B satellite 27.2°.TLE
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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