ZK-2 R/B
Satellite information ZK-2 R/B
| Spacetrack Directory Name | ZK-2 R/B |
| Follow ZK-2 R/B | ZK-2 R/B Tracker |
| Pass predictions ZK-2 R/B | Pass predictions ZK-2 R/B |
| Orbit launches |
2026-11-03 (8 days ago)
|
| Days in orbit | 8 |
| Country/organisation of origin | Chiny (PRC) |
| Starting point | JSC (Jiuquan Satellite Launch Center, China) |
| Perigee | 529 km |
| Apogee | 791 km |
| Orbit slope (inclination) | 88.99° |
| Laps per day | 15 |
| Height ZK-2 R/B | 673.74 km |
Additional information ZK-2 R/B
ZK-2 R/B, 101282 is space debris in LEO originally from a Chinese launch on Tue, 03 Nov 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 ZK-2 R/B Date of exalting 03.11.2026y. Average height of ISS ZK-2 R/B hundred 673.74 km. Average velocity ZK-2 R/B is 27076.43 km/h. Inclination ZK-2 R/B satellite 88.99°.TLE
Average velocity ZK-2 R/B
Average inclination ZK-2 R/B
Mean right ascension of the ascending node (RAAN) ZK-2 R/B
Mean argument of perigee ZK-2 R/B
Mean semi-major axis of the orbit ZK-2 R/B
Mean orbital eccentricity ZK-2 R/B
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