CZ-3 DEB
Satellite information CZ-3 DEB
| Spacetrack Directory Name | CZ-3 DEB |
| Follow CZ-3 DEB | CZ-3 DEB Tracker |
| Pass predictions CZ-3 DEB | Pass predictions CZ-3 DEB |
| Orbit launches |
1986-02-01 (40 years ago)
|
| Days in orbit | 14841 |
| Country/organisation of origin | Chiny (PRC) |
| Starting point | XICLF (Xichang Launch Facility, China) |
| Perigee | 435 km |
| Apogee | 26462 km |
| Orbit slope (inclination) | 31.21° |
| Laps per day | 4 |
| Height CZ-3 DEB | 15484.91 km |
Additional information CZ-3 DEB
CZ-3 DEB, 17425 is space debris in HEO originally from a launch on Sat, 01 Feb 1986 UTC launched from the Xichang Space Center, China (XSC). 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-3 DEB Date of exalting 01.02.1986y. Average height of ISS CZ-3 DEB hundred 15484.91 km. Average velocity CZ-3 DEB is 15007.01 km/h. Inclination CZ-3 DEB satellite 31.21°.TLE
Average velocity CZ-3 DEB
Average inclination CZ-3 DEB
Mean right ascension of the ascending node (RAAN) CZ-3 DEB
Mean argument of perigee CZ-3 DEB
Mean semi-major axis of the orbit CZ-3 DEB
Mean orbital eccentricity CZ-3 DEB
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