ZQ-2E DEB
Satellite information ZQ-2E DEB - ZQ-2E DEB
| Spacetrack Directory Name | ZQ-2E DEB |
| Alternative name | ZQ-2E DEB |
| Orbit launches |
2026-06-09 |
| Deorbitation |
|
| Country/organisation of origin | Chiny (PRC) |
| Starting point | JSC (Jiuquan Satellite Launch Center, China) |
| Perigee | 334 km |
| Apogee | 409 km |
| Height ZQ-2E DEB | 36840579.74 km |
Additional information ZQ-2E DEB
ZQ-2E DEB, 69629 is space debris in LEO originally from a launch on Tue, 09 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 ZQ-2E DEB Date of exalting 09.06.2026y. Average height of ISS ZQ-2E DEB hundred 36840579.74 km. Average velocity ZQ-2E DEB is 605.96 km/h. Inclination ZQ-2E DEB satellite 54.54°.Average velocity ZQ-2E DEB
Average inclination ZQ-2E DEB
Mean right ascension of the ascending node (RAAN) ZQ-2E DEB
Mean argument of perigee ZQ-2E DEB
Mean semi-major axis of the orbit ZQ-2E DEB
Mean orbital eccentricity ZQ-2E DEB
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