QIANFAN-161
Satellite information QIANFAN-161
| Spacetrack Directory Name | QIANFAN-161 |
| Group | QIANFAN |
| Follow QIANFAN-161 | QIANFAN-161 Tracker |
| Group follow QIANFAN | Tracker QIANFAN |
| Pass predictions QIANFAN-161 | Pass predictions QIANFAN-161 |
| Orbit launches |
2026-05-17 (5 months ago)
|
| Days in orbit | 160 |
| Country/organisation of origin | Chiny (PRC) |
| Starting point | WSC (Wenchang Spacecraft Launch Site) |
| Perigee | 815 km |
| Apogee | 834 km |
| Orbit slope (inclination) | 89.02° |
| Laps per day | 14 |
| Height QIANFAN-161 | 1082.24 km |
Additional information QIANFAN-161
QIANFAN-161, 69120 is a Chinese payload satellite in LEO that was launched on Sun, 17 May 2026 UTC via a CHANG ZHENG 8 launch vehicle from the Wenchang Satellite Launch Center (WSC). 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 QIANFAN-161 Date of exalting 17.05.2026y. Average height of ISS QIANFAN-161 hundred 1082.24 km. Average velocity QIANFAN-161 is 26325.32 km/h. Inclination QIANFAN-161 satellite 89.02°.TLE
Average velocity QIANFAN-161
Average inclination QIANFAN-161
Mean right ascension of the ascending node (RAAN) QIANFAN-161
Mean argument of perigee QIANFAN-161
Mean semi-major axis of the orbit QIANFAN-161
Mean orbital eccentricity QIANFAN-161
ISS
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