CZ-12B R/B
Satellite information CZ-12B R/B
| Spacetrack Directory Name | CZ-12B R/B |
| Follow CZ-12B R/B | CZ-12B R/B Tracker |
| Pass predictions CZ-12B R/B | Pass predictions CZ-12B R/B |
| Orbit launches |
2026-06-01 (3 months ago)
|
| Days in orbit | 111 |
| Country/organisation of origin | Chiny (PRC) |
| Starting point | JSC (Jiuquan Satellite Launch Center, China) |
| Perigee | 737 km |
| Apogee | 1022 km |
| Orbit slope (inclination) | 89.03° |
| Laps per day | 14 |
| Height CZ-12B R/B | 893.18 km |
Additional information CZ-12B R/B
CZ-12B R/B, 69327 is space debris in LEO originally from a Chinese launch on Mon, 01 Jun 2026 UTC launched from the Jiuquan Satellite Launch Center, China (JSC). 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-12B R/B Date of exalting 01.06.2026y. Average height of ISS CZ-12B R/B hundred 893.18 km. Average velocity CZ-12B R/B is 26665.63 km/h. Inclination CZ-12B R/B satellite 89.03°.TLE
Average velocity CZ-12B R/B
Average inclination CZ-12B R/B
Mean right ascension of the ascending node (RAAN) CZ-12B R/B
Mean argument of perigee CZ-12B R/B
Mean semi-major axis of the orbit CZ-12B R/B
Mean orbital eccentricity CZ-12B R/B
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