QIANFAN-177
Satellite information QIANFAN-177
| Spacetrack Directory Name | QIANFAN-177 |
| Group | QIANFAN |
| Follow QIANFAN-177 | QIANFAN-177 Tracker |
| Group follow QIANFAN | Tracker QIANFAN |
| Pass predictions QIANFAN-177 | Pass predictions QIANFAN-177 |
| Orbit launches |
2026-06-04 (3 months ago)
|
| Days in orbit | 108 |
| Country/organisation of origin | Chiny (PRC) |
| Starting point | TSC |
| Perigee | 820 km |
| Apogee | 822 km |
| Orbit slope (inclination) | 89.01° |
| Laps per day | 14 |
| Height QIANFAN-177 | 1074.33 km |
Additional information QIANFAN-177
QIANFAN-177, 69394 is a Chinese payload satellite in LEO that was launched on Thu, 04 Jun 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-177 Date of exalting 04.06.2026y. Average height of ISS QIANFAN-177 hundred 1074.33 km. Average velocity QIANFAN-177 is 26339.28 km/h. Inclination QIANFAN-177 satellite 89.01°.TLE
Average velocity QIANFAN-177
Average inclination QIANFAN-177
Mean right ascension of the ascending node (RAAN) QIANFAN-177
Mean argument of perigee QIANFAN-177
Mean semi-major axis of the orbit QIANFAN-177
Mean orbital eccentricity QIANFAN-177
ISS
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