CZ-3 R/B
Satellite information CZ-3 R/B - CZ-3B R/B
| Spacetrack Directory Name | CZ-3 R/B |
| Alternative name | CZ-3B R/B |
| Follow CZ-3 R/B | CZ-3 R/B Tracker |
| Pass predictions CZ-3 R/B | Pass predictions CZ-3 R/B |
| Orbit launches |
2006-10-28 (19 years ago)
|
| Days in orbit | 7248 |
| Country/organisation of origin | Chiny (PRC) |
| Starting point | XICLF (Xichang Launch Facility, China) |
| Perigee | 377 km |
| Apogee | 10231 km |
| Orbit slope (inclination) | 28.24° |
| Laps per day | 7 |
| Height CZ-3 R/B | 6229.32 km |
Additional information CZ-3 R/B
CZ-3 R/B, 29517 is space debris originally from a launch on Sat, 28 Oct 2006 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-3 R/B Date of exalting 28.10.2006y. Average height of ISS CZ-3 R/B hundred 6229.32 km. Average velocity CZ-3 R/B is 20169.96 km/h. Inclination CZ-3 R/B satellite 28.24°.TLE
Average velocity CZ-3 R/B
Average inclination CZ-3 R/B
Mean right ascension of the ascending node (RAAN) CZ-3 R/B
Mean argument of perigee CZ-3 R/B
Mean semi-major axis of the orbit CZ-3 R/B
Mean orbital eccentricity CZ-3 R/B
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