ZK-1A / RB
Satellite information ZK-1A / RB
| Spacetrack Directory Name | ZK-1A / RB |
| Follow ZK-1A / RB | ZK-1A / RB Tracker |
| Pass predictions ZK-1A / RB | Pass predictions ZK-1A / RB |
| Orbit launches |
2026-09-21 (25 days ago)
|
| Days in orbit | 25 |
| Country/organisation of origin | Chiny (PRC) |
| Starting point | JSC (Jiuquan Satellite Launch Center, China) |
| Perigee | 234 km |
| Apogee | 537 km |
| Orbit slope (inclination) | 97.57° |
| Laps per day | 16 |
| Height ZK-1A / RB | 386.08 km |
Additional information ZK-1A / RB
ZK-1A / RB, 100789 is a Chinese payload satellite in SSO that was launched on Mon, 21 Sep 2026 UTC launched from the Jiuquan Satellite Launch Center, China (JSC). Payload-class satellites include a variety of spacecraft equipped with specific instruments for various scientific and technological missions. These include communications satellites like Starlink; space stations such as the ISS; scientific satellites like the Hubble; Earth observation satellites from companies like Planet Labs, Umbra, and HawkEye 360; GPS; miniature CubeSats for education and research; and military/defense satellites.
satellite ZK-1A / RB Date of exalting 21.09.2026y. Average height of ISS ZK-1A / RB hundred 386.08 km. Average velocity ZK-1A / RB is 27647.33 km/h. Inclination ZK-1A / RB satellite 97.57°.TLE
Average velocity ZK-1A / RB
Average inclination ZK-1A / RB
Mean right ascension of the ascending node (RAAN) ZK-1A / RB
Mean argument of perigee ZK-1A / RB
Mean semi-major axis of the orbit ZK-1A / RB
Mean orbital eccentricity ZK-1A / RB
ISS
Buy us a coffee!
