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 |
2026-10-14 (24 days ago)
|
| Days in orbit | 24 |
| Country/organisation of origin | Chiny (PRC) |
| Starting point | JSC (Jiuquan Satellite Launch Center, China) |
| Perigee | 133 km |
| Apogee | 514 km |
| Orbit slope (inclination) | 98.03° |
| Laps per day | 16 |
| Height ZQ-2E R/B | 181.66 km |
Additional information ZQ-2E R/B
ZQ-2E R/B, 101070 is space debris in SSO originally from a launch on Wed, 14 Oct 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 14.10.2026y. Average height of ISS ZQ-2E R/B hundred 181.66 km. Average velocity ZQ-2E R/B is 28077.36 km/h. Inclination ZQ-2E R/B satellite 98.04°.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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