CZ-2D R/B
Satellite information CZ-2D R/B
| Spacetrack Directory Name | CZ-2D R/B |
| Follow CZ-2D R/B | CZ-2D R/B Tracker |
| Pass predictions CZ-2D R/B | Pass predictions CZ-2D R/B |
| Orbit launches |
2013-04-26 (13 years ago)
|
| Days in orbit | 4871 |
| Country/organisation of origin | Chiny (PRC) |
| Starting point | JSC (Jiuquan Satellite Launch Center, China) |
| Perigee | 630 km |
| Apogee | 656 km |
| Orbit slope (inclination) | 98.44° |
| Laps per day | 15 |
| Height CZ-2D R/B | 635.97 km |
Additional information CZ-2D R/B
CZ-2D R/B, 39154 is space debris in SSO originally from a launch on Fri, 26 Apr 2013 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 CZ-2D R/B Date of exalting 26.04.2013y. Average height of ISS CZ-2D R/B hundred 635.97 km. Average velocity CZ-2D R/B is 27150.21 km/h. Inclination CZ-2D R/B satellite 98.44°.TLE
Average velocity CZ-2D R/B
Average inclination CZ-2D R/B
Mean right ascension of the ascending node (RAAN) CZ-2D R/B
Mean argument of perigee CZ-2D R/B
Mean semi-major axis of the orbit CZ-2D R/B
Mean orbital eccentricity CZ-2D R/B
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