QIANFAN-85, 63171
Orbit data source: Space-Track
QIANFAN-85, 63171 is a Chinese payload satellite in LEO that was launched on Tue, 11 Mar 2025 UTC via a CHANG ZHENG 8 launch vehicle from the Wenchang Satellite Launch Center (WSC). 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.
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63171 intel report (Beta)
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TLE from 14 hours ago
0 QIANFAN-85
1 63171U 25046N 25225.89618740 .00000155 00000-0 22129-3 0 9994
2 63171 88.9864 332.3785 0015225 116.2052 244.0667 13.50961508 31153
TLE epoch observation values (Epoch: 2025-08-13T21:30:30.591Z)
Visualization orbit readout
Visualization observer readout
Orbital elements
Other satellites on launch #46 in the year 2025 (2025-03-11 UTC)
QIANFAN-85 Visibility forecast
Observer location: undefined°, undefined°
Span | Click to sort rows by Start time (UTC) header in descending order | Start Az. | Max El. time (UTC) | Max El. Az. | Max El. | End time (UTC) | End Az. |
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5 mins | 2025-08-14 17:41:57.672Z | 51.745° ENE | 2025-08-14 17:43:57.672Z | 70.245° E | 12.529° | 2025-08-14 17:46:57.672Z | 98.109° ESE |
11 mins | 2025-08-14 19:26:57.672Z | 1.367° NNE | 2025-08-14 19:31:57.672Z | 172.758° S | 44.893° | 2025-08-14 19:37:57.672Z | 182.402° SSW |
4 mins | 2025-08-14 21:15:57.672Z | 302.539° NW | 2025-08-14 21:16:57.672Z | 292.842° NW | 13.12° | 2025-08-14 21:19:57.672Z | 264.66° W |
11 mins | 2025-08-15 07:23:57.672Z | 170.68° S | 2025-08-15 07:28:57.672Z | 62.968° ENE | 44.382° | 2025-08-15 07:34:57.672Z | 1.982° NNE |
5 mins | 2025-08-15 09:13:57.672Z | 263.781° W | 2025-08-15 09:15:57.672Z | 283.979° WNW | 15.076° | 2025-08-15 09:18:57.672Z | 313.296° NW |
Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
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Event ID | Pc | Md | Secondary | Secondary name | Country | Click to unsort rows by TCA header |
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