CZ-4 DEB
Satellite information CZ-4 DEB - CZ-4B DEB
| Spacetrack Directory Name | CZ-4 DEB |
| Alternative name | CZ-4B DEB |
| Follow CZ-4 DEB | CZ-4 DEB Tracker |
| Pass predictions CZ-4 DEB | Pass predictions CZ-4 DEB |
| Orbit launches |
1999-10-14 (26 years ago)
|
| Days in orbit | 9819 |
| Country/organisation of origin | Chiny (PRC) |
| Starting point | TAISC (Taiyuan Space Center, China) |
| WWW | Here |
| Perigee | 676 km |
| Apogee | 1084 km |
| Orbit slope (inclination) | 99.08° |
| Laps per day | 14 |
| Height CZ-4 DEB | 857.58 km |
Additional information CZ-4 DEB
CZ-4 DEB, 26162 is space debris in SSO originally from a launch on Thu, 14 Oct 1999 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-4 DEB Date of exalting 14.10.1999y. Average height of ISS CZ-4 DEB hundred 857.58 km. Average velocity CZ-4 DEB is 26730.97 km/h. Inclination CZ-4 DEB satellite 99.08°.TLE
Average velocity CZ-4 DEB
Average inclination CZ-4 DEB
Mean right ascension of the ascending node (RAAN) CZ-4 DEB
Mean argument of perigee CZ-4 DEB
Mean semi-major axis of the orbit CZ-4 DEB
Mean orbital eccentricity CZ-4 DEB
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