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 |
2026-09-24 (one month ago)
|
| Days in orbit | 31 |
| Country/organisation of origin | Chiny (PRC) |
| Starting point | TSC |
| Perigee | 623 km |
| Apogee | 731 km |
| Orbit slope (inclination) | 86.03° |
| Laps per day | 15 |
| Height CZ-6A R/B | 689.4 km |
Additional information CZ-6A R/B
CZ-6A R/B, 100828 is space debris in LEO originally from a Chinese launch on Thu, 24 Sep 2026 UTC launched 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 24.09.2026y. Average height of ISS CZ-6A R/B hundred 689.4 km. Average velocity CZ-6A R/B is 27047.3 km/h. Inclination CZ-6A R/B satellite 86.03°.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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