CHUANG XIN 16A (CX-16A)
Satellite information CHUANG XIN 16A (CX-16A) - 2022-102A
| Spacetrack Directory Name | CHUANG XIN 16A (CX-16A) |
| Alternative name | 2022-102A |
| Follow CHUANG XIN 16A (CX-16A) | CHUANG XIN 16A (CX-16A) Tracker |
| Pass predictions CHUANG XIN 16A (CX-16A) | Pass predictions CHUANG XIN 16A (CX-16A) |
| Orbit launches |
2022-08-23 (3 years ago)
|
| Days in orbit | 1353 |
| Country/organisation of origin | Chiny (PRC) |
| Starting point | XICLF (Xichang Launch Facility, China) |
| Perigee | 590 km |
| Apogee | 596 km |
| Orbit slope (inclination) | 29° |
| Laps per day | 15 |
| Height CHUANG XIN 16A (CX-16A) | 552.53 km |
Additional information CHUANG XIN 16A (CX-16A)
CHUANG XIN 16A (CX-16A), 53586 is a payload satellite owned by IMI/CAS (CN) in LEO that was launched on Tue, 23 Aug 2022 UTC via a KUAIZHOU-1A launch vehicle from the Xichang Space Center, China (XSC). Payloads include a variety of satellites, spacecraft, and rockets 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 CHUANG XIN 16A (CX-16A) Date of exalting 23.08.2022y. Average height of ISS CHUANG XIN 16A (CX-16A) hundred 552.53 km. Average velocity CHUANG XIN 16A (CX-16A) is 27318.45 km/h. Inclination CHUANG XIN 16A (CX-16A) satellite 29°.TLE
Average orbit height CHUANG XIN 16A (CX-16A)
Average velocity CHUANG XIN 16A (CX-16A)
Average inclination CHUANG XIN 16A (CX-16A)
