CZ-6C R/B
Satellite information CZ-6C R/B
| Spacetrack Directory Name | CZ-6C R/B |
| Follow CZ-6C R/B | CZ-6C R/B Tracker |
| Pass predictions CZ-6C R/B | Pass predictions CZ-6C R/B |
| Orbit launches |
2026-08-25 (26 days ago)
|
| Days in orbit | 26 |
| Country/organisation of origin | Chiny (PRC) |
| Starting point | TSC |
| Perigee | 396 km |
| Apogee | 482 km |
| Orbit slope (inclination) | 97.54° |
| Laps per day | 15 |
| Height CZ-6C R/B | 450.52 km |
Additional information CZ-6C R/B
CZ-6C R/B, 100472 is space debris in SSO originally from a Chinese launch on Tue, 25 Aug 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-6C R/B Date of exalting 25.08.2026y. Average height of ISS CZ-6C R/B hundred 450.52 km. Average velocity CZ-6C R/B is 27516.48 km/h. Inclination CZ-6C R/B satellite 97.54°.TLE
Average velocity CZ-6C R/B
Average inclination CZ-6C R/B
Mean right ascension of the ascending node (RAAN) CZ-6C R/B
Mean argument of perigee CZ-6C R/B
Mean semi-major axis of the orbit CZ-6C R/B
Mean orbital eccentricity CZ-6C R/B
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