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 |
1999-05-10 (27 years ago)
|
| Days in orbit | 9972 |
| Country/organisation of origin | Chiny (PRC) |
| Starting point | TAISC (Taiyuan Space Center, China) |
| Categories | |
| Perigee | 806 km |
| Apogee | 860 km |
| Orbit slope (inclination) | 98.64° |
| Laps per day | 14 |
| Height CZ-4B R/B | 843.04 km |
Additional information CZ-4B R/B
CZ-4B R/B, 25732 is space debris in SSO originally from a launch on Mon, 10 May 1999 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 10.05.1999y. Average height of ISS CZ-4B R/B hundred 843.04 km. Average velocity CZ-4B R/B is 26757.97 km/h. Inclination CZ-4B R/B satellite 98.64°.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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