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 |
2015-11-03 (11 years ago)
|
| Days in orbit | 4021 |
| Country/organisation of origin | Chiny (PRC) |
| Starting point | XICLF (Xichang Launch Facility, China) |
| Perigee | 208 km |
| Apogee | 31474 km |
| Orbit slope (inclination) | 26.87° |
| Laps per day | 4 |
| Height CZ-3B R/B | 13727.83 km |
Additional information CZ-3B R/B
CZ-3B R/B, 41022 is space debris in HEO originally from a launch on Tue, 03 Nov 2015 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 03.11.2015y. Average height of ISS CZ-3B R/B hundred 13727.83 km. Average velocity CZ-3B R/B is 15699.22 km/h. Inclination CZ-3B R/B satellite 26.84°.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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