QIANFAN-173
Satellite information QIANFAN-173
| Spacetrack Directory Name | QIANFAN-173 |
| Group | QIANFAN |
| Follow QIANFAN-173 | QIANFAN-173 Tracker |
| Group follow QIANFAN | Tracker QIANFAN |
| Pass predictions QIANFAN-173 | Pass predictions QIANFAN-173 |
| Orbit launches |
2026-06-04 (4 months ago)
|
| Days in orbit | 142 |
| Country/organisation of origin | Chiny (PRC) |
| Starting point | TSC |
| Perigee | 807 km |
| Apogee | 838 km |
| Orbit slope (inclination) | 89° |
| Laps per day | 14 |
| Height QIANFAN-173 | 1080.61 km |
Additional information QIANFAN-173
QIANFAN-173, 69390 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-173 Date of exalting 04.06.2026y. Average height of ISS QIANFAN-173 hundred 1080.61 km. Average velocity QIANFAN-173 is 26328.2 km/h. Inclination QIANFAN-173 satellite 89°.TLE
Average velocity QIANFAN-173
Average inclination QIANFAN-173
Mean right ascension of the ascending node (RAAN) QIANFAN-173
Mean argument of perigee QIANFAN-173
Mean semi-major axis of the orbit QIANFAN-173
Mean orbital eccentricity QIANFAN-173
ISS
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