CHUANGXIN 16B (CX-16B) - Norad ID: 53876
| Nazwa w katalogu Spacetrack | CHUANG XIN 16B (CX-16B) |
| Alternatywna nazwa | CHUANGXIN 16B (CX-16B) |
| Śledź CHUANG XIN 16B (CX-16B) | CHUANG XIN 16B (CX-16B) Tracker |
| Godziny przelotów CHUANG XIN 16B (CX-16B) | Godziny przelotów CHUANG XIN 16B (CX-16B) |
| Wyniesienie na orbitę |
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| Dni na orbicie | 1353 |
| Kraj/organizacja pochodzenia | Chiny (PRC) |
| Miejsce startu | XICLF (Xichang Launch Facility, China) |
| Perygeum | 589 km |
| Apogeum | 596 km |
| Nachylenie orbity (inklinacja) | 28.99° |
| Okrążeń dziennie | 15 |
| Wysokość 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.
Satelitę CHUANG XIN 16B (CX-16B) wyniesiono 23.08.2022r. Średnia wysokość CHUANG XIN 16B (CX-16B) to 479.09 km. Prędkość średnia CHUANG XIN 16B (CX-16B) wynosi 27464.75 km/h. Inklinacja CHUANG XIN 16B (CX-16B) satelity to 28.99°.