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 |
2025-01-06 (one year ago)
|
| Days in orbit | 622 |
| Country/organisation of origin | Chiny (PRC) |
| Starting point | XICLF (Xichang Launch Facility, China) |
| Perigee | 157 km |
| Apogee | 36447 km |
| Orbit slope (inclination) | 28.46° |
| Laps per day | 6 |
| Height CZ-3B R/B | 7472.99 km |
Additional information CZ-3B R/B
CZ-3B R/B, 62486 is space debris in HEO originally from a launch on Mon, 06 Jan 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 06.01.2025y. Average height of ISS CZ-3B R/B hundred 7472.99 km. Average velocity CZ-3B R/B is 19182.42 km/h. Inclination CZ-3B R/B satellite 28.47°.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
ISS
Buy us a coffee!
