CZ-6A R/B
Satellite information CZ-6A R/B
| Spacetrack Directory Name | CZ-6A R/B |
| Follow CZ-6A R/B | CZ-6A R/B Tracker |
| Pass predictions CZ-6A R/B | Pass predictions CZ-6A R/B |
| Orbit launches |
2025-01-23 (one year ago)
|
| Days in orbit | 579 |
| Country/organisation of origin | Chiny (PRC) |
| Starting point | TAISC (Taiyuan Space Center, China) |
| Perigee | 648 km |
| Apogee | 790 km |
| Orbit slope (inclination) | 89° |
| Laps per day | 15 |
| Height CZ-6A R/B | 730 km |
Additional information CZ-6A R/B
CZ-6A R/B, 62803 is space debris in LEO originally from a launch on Thu, 23 Jan 2025 UTC via a CHANG ZHENG 6A launch vehicle from the Taiyaun Space Center, China (TSC). 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-6A R/B Date of exalting 23.01.2025y. Average height of ISS CZ-6A R/B hundred 730 km. Average velocity CZ-6A R/B is 26969.96 km/h. Inclination CZ-6A R/B satellite 89°.TLE
Average velocity CZ-6A R/B
Average inclination CZ-6A R/B
Mean right ascension of the ascending node (RAAN) CZ-6A R/B
Mean argument of perigee CZ-6A R/B
Mean semi-major axis of the orbit CZ-6A R/B
Mean orbital eccentricity CZ-6A R/B
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