CZ-6A DEB
Satellite information CZ-6A DEB
| Spacetrack Directory Name | CZ-6A DEB |
| Follow CZ-6A DEB | CZ-6A DEB Tracker |
| Pass predictions CZ-6A DEB | Pass predictions CZ-6A DEB |
| Orbit launches |
2026-07-30 (25 days ago)
|
| Days in orbit | 25 |
| Country/organisation of origin | Chiny (PRC) |
| Starting point | TSC |
| Perigee | 1148 km |
| Apogee | 1160 km |
| Orbit slope (inclination) | 64.79° |
| Laps per day | 13 |
| Height CZ-6A DEB | 1163.7 km |
Additional information CZ-6A DEB
CZ-6A DEB, 100175 is space debris in LEO originally from a Chinese launch on Thu, 30 Jul 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 DEB Date of exalting 30.07.2026y. Average height of ISS CZ-6A DEB hundred 1163.7 km. Average velocity CZ-6A DEB is 26183.5 km/h. Inclination CZ-6A DEB satellite 64.79°.TLE
Average velocity CZ-6A DEB
Average inclination CZ-6A DEB
Mean right ascension of the ascending node (RAAN) CZ-6A DEB
Mean argument of perigee CZ-6A DEB
Mean semi-major axis of the orbit CZ-6A DEB
Mean orbital eccentricity CZ-6A DEB
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