CZ-4B R/B
Satellite information CZ-4B R/B
| Spacetrack Directory Name | CZ-4B R/B |
| Follow CZ-4B R/B | CZ-4B R/B Tracker |
| Pass predictions CZ-4B R/B | Pass predictions CZ-4B R/B |
| Orbit launches |
2024-11-13 (one year ago)
|
| Days in orbit | 652 |
| Country/organisation of origin | Chiny (PRC) |
| Starting point | TAISC (Taiyuan Space Center, China) |
| Perigee | 411 km |
| Apogee | 631 km |
| Orbit slope (inclination) | 97.94° |
| Laps per day | 15 |
| Height CZ-4B R/B | 488.53 km |
Additional information CZ-4B R/B
CZ-4B R/B, 61938 is space debris in SSO originally from a launch on Wed, 13 Nov 2024 UTC launched from the Taiyaun Space Center, China (TSC). 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-4B R/B Date of exalting 13.11.2024y. Average height of ISS CZ-4B R/B hundred 488.53 km. Average velocity CZ-4B R/B is 27440.63 km/h. Inclination CZ-4B R/B satellite 97.94°.TLE
Average velocity CZ-4B R/B
Average inclination CZ-4B R/B
Mean right ascension of the ascending node (RAAN) CZ-4B R/B
Mean argument of perigee CZ-4B R/B
Mean semi-major axis of the orbit CZ-4B R/B
Mean orbital eccentricity CZ-4B R/B
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