CZ-2F R/B
Satellite information CZ-2F R/B
| Spacetrack Directory Name | CZ-2F R/B |
| Follow CZ-2F R/B | CZ-2F R/B Tracker |
| Pass predictions CZ-2F R/B | Pass predictions CZ-2F R/B |
| Orbit launches |
2026-02-07 (7 months ago)
|
| Days in orbit | 225 |
| Country/organisation of origin | Chiny (PRC) |
| Starting point | JSC (Jiuquan Satellite Launch Center, China) |
| Perigee | 343 km |
| Apogee | 577 km |
| Orbit slope (inclination) | 49.98° |
| Laps per day | 15 |
| Height CZ-2F R/B | 451.37 km |
Additional information CZ-2F R/B
CZ-2F R/B, 67690 is space debris in LEO originally from a launch on Sat, 07 Feb 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-2F R/B Date of exalting 07.02.2026y. Average height of ISS CZ-2F R/B hundred 451.37 km. Average velocity CZ-2F R/B is 27517.83 km/h. Inclination CZ-2F R/B satellite 49.98°.TLE
Average velocity CZ-2F R/B
Average inclination CZ-2F R/B
Mean right ascension of the ascending node (RAAN) CZ-2F R/B
Mean argument of perigee CZ-2F R/B
Mean semi-major axis of the orbit CZ-2F R/B
Mean orbital eccentricity CZ-2F R/B
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