YZ-1S R/B
Satellite information YZ-1S R/B - 0 YZ-1S R/B
| Spacetrack Directory Name | YZ-1S R/B |
| Alternative name | 0 YZ-1S R/B |
| Follow YZ-1S R/B | YZ-1S R/B Tracker |
| Pass predictions YZ-1S R/B | Pass predictions YZ-1S R/B |
| Orbit launches |
2024-03-13 (2 years ago)
|
| Days in orbit | 902 |
| Country/organisation of origin | Chiny (PRC) |
| Starting point | XICLF (Xichang Launch Facility, China) |
| Perigee | 1086 km |
| Apogee | 125242 km |
| Orbit slope (inclination) | 15.48° |
| Laps per day | 0 |
| Height YZ-1S R/B | 89428.56 km |
Additional information YZ-1S R/B
YZ-1S R/B, 60326 is space debris in HEO originally from a launch on Wed, 13 Mar 2024 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 YZ-1S R/B Date of exalting 13.03.2024y. Average height of ISS YZ-1S R/B hundred 89428.56 km. Average velocity YZ-1S R/B is 6667.7 km/h. Inclination YZ-1S R/B satellite 15.55°.TLE
Average velocity YZ-1S R/B
Average inclination YZ-1S R/B
Mean right ascension of the ascending node (RAAN) YZ-1S R/B
Mean argument of perigee YZ-1S R/B
Mean semi-major axis of the orbit YZ-1S R/B
Mean orbital eccentricity YZ-1S R/B
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