ZK-1A R/B
Satellite information ZK-1A R/B
| Spacetrack Directory Name | ZK-1A R/B |
| Follow ZK-1A R/B | ZK-1A R/B Tracker |
| Pass predictions ZK-1A R/B | Pass predictions ZK-1A R/B |
| Orbit launches |
2025-11-09 (10 months ago)
|
| Days in orbit | 315 |
| Country/organisation of origin | Chiny (PRC) |
| Starting point | JSC (Jiuquan Satellite Launch Center, China) |
| Perigee | 402 km |
| Apogee | 724 km |
| Orbit slope (inclination) | 98.3° |
| Laps per day | 15 |
| Height ZK-1A R/B | 550.26 km |
Additional information ZK-1A R/B
ZK-1A R/B, 66411 is space debris in SSO originally from a launch on Sun, 09 Nov 2025 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 ZK-1A R/B Date of exalting 09.11.2025y. Average height of ISS ZK-1A R/B hundred 550.26 km. Average velocity ZK-1A R/B is 27317.81 km/h. Inclination ZK-1A R/B satellite 98.3°.TLE
Average velocity ZK-1A R/B
Average inclination ZK-1A R/B
Mean right ascension of the ascending node (RAAN) ZK-1A R/B
Mean argument of perigee ZK-1A R/B
Mean semi-major axis of the orbit ZK-1A R/B
Mean orbital eccentricity ZK-1A R/B
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