CZ-8 R/B
Satellite information CZ-8 R/B
| Spacetrack Directory Name | CZ-8 R/B |
| Follow CZ-8 R/B | CZ-8 R/B Tracker |
| Pass predictions CZ-8 R/B | Pass predictions CZ-8 R/B |
| Orbit launches |
2026-06-05 (2 months ago)
|
| Days in orbit | 81 |
| Country/organisation of origin | Chiny (PRC) |
| Starting point | WSC (Wenchang Spacecraft Launch Site) |
| Perigee | 726 km |
| Apogee | 829 km |
| Orbit slope (inclination) | 88.99° |
| Laps per day | 14 |
| Height CZ-8 R/B | 771.24 km |
Additional information CZ-8 R/B
CZ-8 R/B, 69419 is space debris in LEO originally from a launch on Fri, 05 Jun 2026 UTC launched from the Wenchang Satellite Launch Center (WSC). 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-8 R/B Date of exalting 05.06.2026y. Average height of ISS CZ-8 R/B hundred 771.24 km. Average velocity CZ-8 R/B is 26892 km/h. Inclination CZ-8 R/B satellite 88.99°.TLE
Average velocity CZ-8 R/B
Average inclination CZ-8 R/B
Mean right ascension of the ascending node (RAAN) CZ-8 R/B
Mean argument of perigee CZ-8 R/B
Mean semi-major axis of the orbit CZ-8 R/B
Mean orbital eccentricity CZ-8 R/B
ISS
Buy us a coffee!
