ZQ-2E R/B
Satellite information ZQ-2E R/B
| Spacetrack Directory Name | ZQ-2E R/B |
| Follow ZQ-2E R/B | ZQ-2E R/B Tracker |
| Pass predictions ZQ-2E R/B | Pass predictions ZQ-2E R/B |
| Orbit launches |
2026-06-09 (3 months ago)
|
| Days in orbit | 103 |
| Country/organisation of origin | Chiny (PRC) |
| Starting point | JSC (Jiuquan Satellite Launch Center, China) |
| Perigee | 335 km |
| Apogee | 425 km |
| Orbit slope (inclination) | 54.52° |
| Laps per day | 16 |
| Height ZQ-2E R/B | 362.4 km |
Additional information ZQ-2E R/B
ZQ-2E R/B, 69537 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 R/B Date of exalting 09.06.2026y. Average height of ISS ZQ-2E R/B hundred 362.4 km. Average velocity ZQ-2E R/B is 27698.39 km/h. Inclination ZQ-2E R/B satellite 54.53°.TLE
Average velocity ZQ-2E R/B
Average inclination ZQ-2E R/B
Mean right ascension of the ascending node (RAAN) ZQ-2E R/B
Mean argument of perigee ZQ-2E R/B
Mean semi-major axis of the orbit ZQ-2E R/B
Mean orbital eccentricity ZQ-2E R/B
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