CZ-4B DEB
Satellite information CZ-4B DEB
| Spacetrack Directory Name | CZ-4B DEB |
| Follow CZ-4B DEB | CZ-4B DEB Tracker |
| Pass predictions CZ-4B DEB | Pass predictions CZ-4B DEB |
| Orbit launches |
2002-05-15 (24 years ago)
|
| Days in orbit | 8875 |
| Country/organisation of origin | Chiny (PRC) |
| Starting point | TAISC (Taiyuan Space Center, China) |
| Perigee | 839 km |
| Apogee | 1178 km |
| Orbit slope (inclination) | 98.85° |
| Laps per day | 14 |
| Height CZ-4B DEB | 1015.7 km |
Additional information CZ-4B DEB
CZ-4B DEB, 29216 is space debris in SSO originally from a launch on Wed, 15 May 2002 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-4B DEB Date of exalting 15.05.2002y. Average height of ISS CZ-4B DEB hundred 1015.7 km. Average velocity CZ-4B DEB is 26443.58 km/h. Inclination CZ-4B DEB satellite 98.85°.TLE
Average velocity CZ-4B DEB
Average inclination CZ-4B DEB
Mean right ascension of the ascending node (RAAN) CZ-4B DEB
Mean argument of perigee CZ-4B DEB
Mean semi-major axis of the orbit CZ-4B DEB
Mean orbital eccentricity CZ-4B DEB
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