CZ-12 R/B
Satellite information CZ-12 R/B
| Spacetrack Directory Name | CZ-12 R/B |
| Follow CZ-12 R/B | CZ-12 R/B Tracker |
| Pass predictions CZ-12 R/B | Pass predictions CZ-12 R/B |
| Orbit launches |
2024-11-30 (one year ago)
|
| Days in orbit | 634 |
| Country/organisation of origin | Chiny (PRC) |
| Starting point | WSC (Wenchang Spacecraft Launch Site) |
| Perigee | 942 km |
| Apogee | 1032 km |
| Orbit slope (inclination) | 50° |
| Laps per day | 14 |
| Height CZ-12 R/B | 992.51 km |
Additional information CZ-12 R/B
CZ-12 R/B, 62187 is space debris in LEO originally from a launch on Sat, 30 Nov 2024 UTC via a CHANG ZHENG 12 launch vehicle 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-12 R/B Date of exalting 30.11.2024y. Average height of ISS CZ-12 R/B hundred 992.51 km. Average velocity CZ-12 R/B is 26487.34 km/h. Inclination CZ-12 R/B satellite 50°.TLE
Average velocity CZ-12 R/B
Average inclination CZ-12 R/B
Mean right ascension of the ascending node (RAAN) CZ-12 R/B
Mean argument of perigee CZ-12 R/B
Mean semi-major axis of the orbit CZ-12 R/B
Mean orbital eccentricity CZ-12 R/B
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