QIANFAN-158
Satellite information QIANFAN-158
| Spacetrack Directory Name | QIANFAN-158 |
| Group | QIANFAN |
| Follow QIANFAN-158 | QIANFAN-158 Tracker |
| Group follow QIANFAN | Tracker QIANFAN |
| Pass predictions QIANFAN-158 | Pass predictions QIANFAN-158 |
| 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 | 816 km |
| Apogee | 839 km |
| Orbit slope (inclination) | 89.02° |
| Laps per day | 14 |
| Height QIANFAN-158 | 1085.78 km |
Additional information QIANFAN-158
QIANFAN-158, 69117 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-158 Date of exalting 17.05.2026y. Average height of ISS QIANFAN-158 hundred 1085.78 km. Average velocity QIANFAN-158 is 26319.1 km/h. Inclination QIANFAN-158 satellite 89.02°.TLE
Average velocity QIANFAN-158
Average inclination QIANFAN-158
Mean right ascension of the ascending node (RAAN) QIANFAN-158
Mean argument of perigee QIANFAN-158
Mean semi-major axis of the orbit QIANFAN-158
Mean orbital eccentricity QIANFAN-158
ISS
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