QIANFAN-144
Satellite information QIANFAN-144 - QIANFAN-145
| Spacetrack Directory Name | QIANFAN-144 |
| Alternative name | QIANFAN-145 |
| Group | QIANFAN |
| Follow QIANFAN-144 | QIANFAN-144 Tracker |
| Group follow QIANFAN | Tracker QIANFAN |
| Pass predictions QIANFAN-144 | Pass predictions QIANFAN-144 |
| Orbit launches |
2026-05-12 (4 months ago)
|
| Days in orbit | 131 |
| Country/organisation of origin | Chiny (PRC) |
| Starting point | TSC |
| Perigee | 818 km |
| Apogee | 820 km |
| Orbit slope (inclination) | 88.99° |
| Laps per day | 14 |
| Height QIANFAN-144 | 1080.98 km |
Additional information QIANFAN-144
QIANFAN-145, 69090 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-144 Date of exalting 12.05.2026y. Average height of ISS QIANFAN-144 hundred 1080.98 km. Average velocity QIANFAN-144 is 26327.56 km/h. Inclination QIANFAN-144 satellite 88.99°.TLE
Average velocity QIANFAN-144
Average inclination QIANFAN-144
Mean right ascension of the ascending node (RAAN) QIANFAN-144
Mean argument of perigee QIANFAN-144
Mean semi-major axis of the orbit QIANFAN-144
Mean orbital eccentricity QIANFAN-144
ISS
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