QIANFAN-140
Satellite information QIANFAN-140 - QIANFAN-141
| Spacetrack Directory Name | QIANFAN-140 |
| Alternative name | QIANFAN-141 |
| Group | QIANFAN |
| Follow QIANFAN-140 | QIANFAN-140 Tracker |
| Group follow QIANFAN | Tracker QIANFAN |
| Pass predictions QIANFAN-140 | Pass predictions QIANFAN-140 |
| Orbit launches |
2026-05-12 (4 months ago)
|
| Days in orbit | 131 |
| Country/organisation of origin | Chiny (PRC) |
| Starting point | TSC |
| Perigee | 814 km |
| Apogee | 826 km |
| Orbit slope (inclination) | 88.99° |
| Laps per day | 14 |
| Height QIANFAN-140 | 1081.36 km |
Additional information QIANFAN-140
QIANFAN-141, 69086 is a Chinese payload satellite in LEO that was launched on Tue, 12 May 2026 UTC via a CHANG ZHENG 6A launch vehicle from the Taiyaun Space Center, China (TSC). 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-140 Date of exalting 12.05.2026y. Average height of ISS QIANFAN-140 hundred 1081.36 km. Average velocity QIANFAN-140 is 26326.87 km/h. Inclination QIANFAN-140 satellite 88.99°.TLE
Average velocity QIANFAN-140
Average inclination QIANFAN-140
Mean right ascension of the ascending node (RAAN) QIANFAN-140
Mean argument of perigee QIANFAN-140
Mean semi-major axis of the orbit QIANFAN-140
Mean orbital eccentricity QIANFAN-140
ISS
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