YZ-1 R/B
Rocket
Satellite information YZ-1 R/B - Satelita
| Spacetrack Directory Name | YZ-1 R/B |
| Alternative name | Satelita |
| Follow YZ-1 R/B | YZ-1 R/B Tracker |
| Pass predictions YZ-1 R/B | Pass predictions YZ-1 R/B |
| Country/organisation of origin | Chiny (PRC) |
| Starting point | |
| Perigee | 36002 km |
| Apogee | 36818 km |
| Orbit slope (inclination) | 28.87° |
| Laps per day | 1 |
| Height YZ-1 R/B | 36415.02 km |
Additional information YZ-1 R/B
YZ-1 R/B, 66553 is space debris in GEO originally from a launch on Fri, 05 Sep 2025 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.
Average height of ISS YZ-1 R/B hundred 36415.02 km. Average velocity YZ-1 R/B is 10987.47 km/h. Inclination YZ-1 R/B satellite 28.81°.TLE
Average velocity YZ-1 R/B
Average inclination YZ-1 R/B
Mean right ascension of the ascending node (RAAN) YZ-1 R/B
Mean argument of perigee YZ-1 R/B
Mean semi-major axis of the orbit YZ-1 R/B
Mean orbital eccentricity YZ-1 R/B
ISS
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