CZ-2F DEB
Satellite information CZ-2F DEB
| Spacetrack Directory Name | CZ-2F DEB |
| Follow CZ-2F DEB | CZ-2F DEB Tracker |
| Pass predictions CZ-2F DEB | Pass predictions CZ-2F DEB |
| Orbit launches |
2026-02-07 (6 months ago)
|
| Days in orbit | 200 |
| Country/organisation of origin | Chiny (PRC) |
| Starting point | JSC (Jiuquan Satellite Launch Center, China) |
| Perigee | 337 km |
| Apogee | 737 km |
| Orbit slope (inclination) | 49.8° |
| Laps per day | 16 |
| Height CZ-2F DEB | 330.19 km |
Additional information CZ-2F DEB
CZ-2F DEB, 67720 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 DEB Date of exalting 07.02.2026y. Average height of ISS CZ-2F DEB hundred 330.19 km. Average velocity CZ-2F DEB is 27765.44 km/h. Inclination CZ-2F DEB satellite 49.8°.TLE
Average velocity CZ-2F DEB
Average inclination CZ-2F DEB
Mean right ascension of the ascending node (RAAN) CZ-2F DEB
Mean argument of perigee CZ-2F DEB
Mean semi-major axis of the orbit CZ-2F DEB
Mean orbital eccentricity CZ-2F DEB
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