ZQ-2E DEB
Satellite information ZQ-2E DEB
| Spacetrack Directory Name | ZQ-2E DEB |
| Follow ZQ-2E DEB | ZQ-2E DEB Tracker |
| Pass predictions ZQ-2E DEB | Pass predictions ZQ-2E DEB |
| Orbit launches |
2026-06-09 (2 months ago)
|
| Days in orbit | 73 |
| Country/organisation of origin | Chiny (PRC) |
| Starting point | JSC (Jiuquan Satellite Launch Center, China) |
| Perigee | 341 km |
| Apogee | 445 km |
| Orbit slope (inclination) | 54.53° |
| Laps per day | 16 |
| Height ZQ-2E DEB | 394.79 km |
Additional information ZQ-2E DEB
ZQ-2E DEB, 69630 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 394.79 km. Average velocity ZQ-2E DEB is 27632.1 km/h. Inclination ZQ-2E DEB satellite 54.53°.TLE
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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