CZ-7A R/B
Satellite information CZ-7A R/B
| Spacetrack Directory Name | CZ-7A R/B |
| Orbit launches |
2026-07-29 |
| Deorbitation |
|
| Country/organisation of origin | Chiny (PRC) |
| Starting point | WSC (Wenchang Spacecraft Launch Site) |
| Perigee | 154 km |
| Apogee | 34289 km |
| Height CZ-7A R/B | 22582.78 km |
Additional information CZ-7A R/B
CZ-7A R/B, 100173 is space debris in HEO originally from a Chinese launch on Wed, 29 Jul 2026 UTC launched from the Wenchang Satellite Launch Center (WSC). 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-7A R/B Date of exalting 29.07.2026y. Average height of ISS CZ-7A R/B hundred 22582.78 km. Average velocity CZ-7A R/B is 12808.57 km/h. Inclination CZ-7A R/B satellite 15.45°.Average velocity CZ-7A R/B
Average inclination CZ-7A R/B
Mean right ascension of the ascending node (RAAN) CZ-7A R/B
Mean argument of perigee CZ-7A R/B
Mean semi-major axis of the orbit CZ-7A R/B
Mean orbital eccentricity CZ-7A R/B
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