QIANFAN-256
Satellite information QIANFAN-256
| Spacetrack Directory Name | QIANFAN-256 |
| Group | QIANFAN |
| Follow QIANFAN-256 | QIANFAN-256 Tracker |
| Group follow QIANFAN | Tracker QIANFAN |
| Pass predictions QIANFAN-256 | Pass predictions QIANFAN-256 |
| Orbit launches |
2026-11-03 (8 days ago)
|
| Days in orbit | 8 |
| Country/organisation of origin | Chiny (PRC) |
| Starting point | JSC (Jiuquan Satellite Launch Center, China) |
| Perigee | 796 km |
| Apogee | 804 km |
| Orbit slope (inclination) | 88.99° |
| Laps per day | 14 |
| Height QIANFAN-256 | 812.44 km |
Additional information QIANFAN-256
QIANFAN-256, 101271 is a Chinese payload satellite in LEO that was launched on Tue, 03 Nov 2026 UTC via a LIJIAN-2 launch vehicle from the Jiuquan Satellite Launch Center, China (JSC). 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-256 Date of exalting 03.11.2026y. Average height of ISS QIANFAN-256 hundred 812.44 km. Average velocity QIANFAN-256 is 26814.65 km/h. Inclination QIANFAN-256 satellite 88.99°.TLE
Average velocity QIANFAN-256
Average inclination QIANFAN-256
Mean right ascension of the ascending node (RAAN) QIANFAN-256
Mean argument of perigee QIANFAN-256
Mean semi-major axis of the orbit QIANFAN-256
Mean orbital eccentricity QIANFAN-256
ISS
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