2024-170D
Satellite information 2024-170D
| Spacetrack Directory Name | 2024-170D |
| Follow 2024-170D | 2024-170D Tracker |
| Pass predictions 2024-170D | Pass predictions 2024-170D |
| Orbit launches |
2024-09-20 (one year ago)
|
| Days in orbit | 707 |
| Country/organisation of origin | Chiny (PRC) |
| Starting point | XICLF (Xichang Launch Facility, China) |
| Perigee | 842 km |
| Apogee | 854 km |
| Orbit slope (inclination) | 44.86° |
| Laps per day | 14 |
| Height 2024-170D | 902.33 km |
Additional information 2024-170D
TIANQI 32, 61198 is a payload satellite owned by Guodian Gaokeji (CN) in LEO that was launched on Fri, 20 Sep 2024 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 2024-170D Date of exalting 20.09.2024y. Average height of ISS 2024-170D hundred 902.33 km. Average velocity 2024-170D is 26651.38 km/h. Inclination 2024-170D satellite 44.86°.TLE
Average velocity 2024-170D
Average inclination 2024-170D
Mean right ascension of the ascending node (RAAN) 2024-170D
Mean argument of perigee 2024-170D
Mean semi-major axis of the orbit 2024-170D
Mean orbital eccentricity 2024-170D
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