CZ-2D R/B
Satellite information CZ-2D R/B
| Spacetrack Directory Name | CZ-2D R/B |
| Follow CZ-2D R/B | CZ-2D R/B Tracker |
| Pass predictions CZ-2D R/B | Pass predictions CZ-2D R/B |
| Orbit launches |
2022-10-29 (3 years ago)
|
| Days in orbit | 1459 |
| Country/organisation of origin | Chiny (PRC) |
| Starting point | JSC (Jiuquan Satellite Launch Center, China) |
| Perigee | 762 km |
| Apogee | 798 km |
| Orbit slope (inclination) | 59.9° |
| Laps per day | 14 |
| Height CZ-2D R/B | 785.55 km |
Additional information CZ-2D R/B
CZ-2D R/B, 54215 is space debris in LEO originally from a launch on Sat, 29 Oct 2022 UTC launched from the Jiuquan Satellite Launch Center, China (JSC). 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-2D R/B Date of exalting 29.10.2022y. Average height of ISS CZ-2D R/B hundred 785.55 km. Average velocity CZ-2D R/B is 26866.55 km/h. Inclination CZ-2D R/B satellite 59.9°.TLE
Average velocity CZ-2D R/B
Average inclination CZ-2D R/B
Mean right ascension of the ascending node (RAAN) CZ-2D R/B
Mean argument of perigee CZ-2D R/B
Mean semi-major axis of the orbit CZ-2D R/B
Mean orbital eccentricity CZ-2D R/B
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