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 |
2018-10-24 (7 years ago)
|
| Days in orbit | 2859 |
| Country/organisation of origin | Chiny (PRC) |
| Starting point | TAISC (Taiyuan Space Center, China) |
| WWW | Here |
| Perigee | 641 km |
| Apogee | 939 km |
| Orbit slope (inclination) | 99.36° |
| Laps per day | 14 |
| Orbit | LEO (Sun-Synchronous) |
| Height CZ-4B R/B | 798.6 km |
Additional information CZ-4B R/B
CZ-4B R/B, 43656 is space debris in SSO originally from a launch on Wed, 24 Oct 2018 UTC via a CHANG ZHENG 4B launch vehicle 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 24.10.2018y. Average height of ISS CZ-4B R/B hundred 798.6 km. Average velocity CZ-4B R/B is 26841.36 km/h. Inclination CZ-4B R/B satellite 99.36°.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
Frequency CZ-4B R/B
In the table below we show the frequencies CZ-4B R/B.
| Downlink | Mode |
|---|---|
| 432.084 MHz | FM |
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