CZ-3B R/B
Satellite information CZ-3B R/B - 0 CZ-3B R/B
| Spacetrack Directory Name | CZ-3B R/B |
| Alternative name | 0 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 |
2024-02-29 (2 years ago)
|
| Days in orbit | 915 |
| Country/organisation of origin | Chiny (PRC) |
| Starting point | XICLF (Xichang Launch Facility, China) |
| Perigee | 155 km |
| Apogee | 22459 km |
| Orbit slope (inclination) | 27.23° |
| Laps per day | 4 |
| Height CZ-3B R/B | 14720.8 km |
Additional information CZ-3B R/B
CZ-3B R/B, 59070 is space debris in HEO originally from a launch on Thu, 29 Feb 2024 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 29.02.2024y. Average height of ISS CZ-3B R/B hundred 14720.8 km. Average velocity CZ-3B R/B is 15297.71 km/h. Inclination CZ-3B R/B satellite 27.24°.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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