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 |
2024-05-30 (2 years ago)
|
| Days in orbit | 822 |
| Country/organisation of origin | Chiny (PRC) |
| Starting point | XICLF (Xichang Launch Facility, China) |
| Perigee | 164 km |
| Apogee | 34336 km |
| Orbit slope (inclination) | 26.7° |
| Laps per day | 3 |
| Height CZ-3B R/B | 16460 km |
Additional information CZ-3B R/B
CZ-3B R/B, 59916 is space debris in HEO originally from a launch on Thu, 30 May 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 30.05.2024y. Average height of ISS CZ-3B R/B hundred 16460 km. Average velocity CZ-3B R/B is 14644.08 km/h. Inclination CZ-3B R/B satellite 26.69°.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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