CHUANGXIN 16B (CX-16B) - Norad ID: 53876
| Spacetrack Directory Name | CHUANG XIN 16B (CX-16B) |
| Alternative name | CHUANGXIN 16B (CX-16B) |
| Follow CHUANG XIN 16B (CX-16B) | CHUANG XIN 16B (CX-16B) Tracker |
| Pass predictions CHUANG XIN 16B (CX-16B) | Pass predictions CHUANG XIN 16B (CX-16B) |
| Orbit launches |
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| Days in orbit | 1353 |
| Country/organisation of origin | Chiny (PRC) |
| Starting point | XICLF (Xichang Launch Facility, China) |
| Perigee | 589 km |
| Apogee | 596 km |
| Orbit slope (inclination) | 28.99° |
| Laps per day | 15 |
| Height CHUANG XIN 16B (CX-16B) | 479.09 km |
CHUANG XIN 16B (CX-16B), 53876 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 16B (CX-16B) Date of exalting 23.08.2022y. Average height of ISS CHUANG XIN 16B (CX-16B) hundred 479.09 km. Average velocity CHUANG XIN 16B (CX-16B) is 27464.75 km/h. Inclination CHUANG XIN 16B (CX-16B) satellite 28.99°.