QIANFAN-159
Satellite information QIANFAN-159
| Spacetrack Directory Name | QIANFAN-159 |
| Group | QIANFAN |
| Follow QIANFAN-159 | QIANFAN-159 Tracker |
| Group follow QIANFAN | Tracker QIANFAN |
| Pass predictions QIANFAN-159 | Pass predictions QIANFAN-159 |
| Orbit launches |
2026-05-17 (4 months ago)
|
| Days in orbit | 126 |
| Country/organisation of origin | Chiny (PRC) |
| Starting point | WSC (Wenchang Spacecraft Launch Site) |
| Perigee | 815 km |
| Apogee | 837 km |
| Orbit slope (inclination) | 89.02° |
| Laps per day | 14 |
| Height QIANFAN-159 | 1081.73 km |
Additional information QIANFAN-159
QIANFAN-159, 69118 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-159 Date of exalting 17.05.2026y. Average height of ISS QIANFAN-159 hundred 1081.73 km. Average velocity QIANFAN-159 is 26326.21 km/h. Inclination QIANFAN-159 satellite 89.01°.TLE
Average velocity QIANFAN-159
Average inclination QIANFAN-159
Mean right ascension of the ascending node (RAAN) QIANFAN-159
Mean argument of perigee QIANFAN-159
Mean semi-major axis of the orbit QIANFAN-159
Mean orbital eccentricity QIANFAN-159
ISS
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