YZ-2 R/B
Satellite information YZ-2 R/B
| Spacetrack Directory Name | YZ-2 R/B |
| Follow YZ-2 R/B | YZ-2 R/B Tracker |
| Pass predictions YZ-2 R/B | Pass predictions YZ-2 R/B |
| Orbit launches |
2016-11-03 (10 years ago)
|
| Days in orbit | 3657 |
| Country/organisation of origin | Chiny (PRC) |
| Starting point | WSC (Wenchang Spacecraft Launch Site) |
| Perigee | 35609 km |
| Apogee | 40004 km |
| Orbit slope (inclination) | 9.75° |
| Laps per day | 1 |
| Height YZ-2 R/B | 37855.78 km |
Additional information YZ-2 R/B
YZ-2 R/B, 41840 is space debris in GEO originally from a launch on Thu, 03 Nov 2016 UTC launched from the Wenchang Satellite Launch Center (WSC). 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 YZ-2 R/B Date of exalting 03.11.2016y. Average height of ISS YZ-2 R/B hundred 37855.78 km. Average velocity YZ-2 R/B is 10806.65 km/h. Inclination YZ-2 R/B satellite 9.63°.TLE
Average velocity YZ-2 R/B
Average inclination YZ-2 R/B
Mean right ascension of the ascending node (RAAN) YZ-2 R/B
Mean argument of perigee YZ-2 R/B
Mean semi-major axis of the orbit YZ-2 R/B
Mean orbital eccentricity YZ-2 R/B
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