SJ 16-02 DEB
Satellite information SJ 16-02 DEB
| Spacetrack Directory Name | SJ 16-02 DEB |
| Follow SJ 16-02 DEB | SJ 16-02 DEB Tracker |
| Pass predictions SJ 16-02 DEB | Pass predictions SJ 16-02 DEB |
| Orbit launches |
2016-06-29 (10 years ago)
|
| Days in orbit | 3782 |
| Country/organisation of origin | Chiny (PRC) |
| Starting point | JSC (Jiuquan Satellite Launch Center, China) |
| WWW | Here |
| Perigee | 600 km |
| Apogee | 1009 km |
| Orbit slope (inclination) | 74.96° |
| Laps per day | 14 |
| Height SJ 16-02 DEB | 769.3 km |
Additional information SJ 16-02 DEB
SJ 16-02 DEB, 43428 is space debris in LEO originally from a launch on Wed, 29 Jun 2016 UTC launched from the Jiuquan Satellite Launch Center, China (JSC). 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 SJ 16-02 DEB Date of exalting 29.06.2016y. Average height of ISS SJ 16-02 DEB hundred 769.3 km. Average velocity SJ 16-02 DEB is 26896.04 km/h. Inclination SJ 16-02 DEB satellite 74.96°.TLE
Average velocity SJ 16-02 DEB
Average inclination SJ 16-02 DEB
Mean right ascension of the ascending node (RAAN) SJ 16-02 DEB
Mean argument of perigee SJ 16-02 DEB
Mean semi-major axis of the orbit SJ 16-02 DEB
Mean orbital eccentricity SJ 16-02 DEB
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