QIANFAN-83, 63169
Orbit data source: Space-Track
QIANFAN-83, 63169 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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63169 intel report (Beta)
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TLE from 1 day ago
0 QIANFAN-83
1 63169U 25046L 25224.74231837 .00000204 00000-0 24926-3 0 9994
2 63169 88.9864 332.5067 0016184 112.8869 247.3999 13.61934962 30999
TLE epoch observation values (Epoch: 2025-08-12T17:48:56.307Z)
Visualization orbit readout
Visualization observer readout
Orbital elements
Other satellites on launch #46 in the year 2025 (2025-03-11 UTC)
QIANFAN-83 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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6 mins | 2025-08-13 19:10:48.107Z | 75.158° E | 2025-08-13 19:10:48.107Z | 75.158° E | 39.9° | 2025-08-13 19:16:48.107Z | 164.837° S |
8 mins | 2025-08-13 20:52:48.107Z | 323.289° NNW | 2025-08-13 20:55:48.107Z | 290.984° WNW | 19.849° | 2025-08-13 21:00:48.107Z | 238.801° WSW |
10 mins | 2025-08-14 06:57:48.107Z | 147.099° SSE | 2025-08-14 07:02:48.107Z | 74.852° E | 35.17° | 2025-08-14 07:07:48.107Z | 14.484° NNE |
8 mins | 2025-08-14 08:44:48.107Z | 234.576° WSW | 2025-08-14 08:48:48.107Z | 285.571° WNW | 24.34° | 2025-08-14 08:52:48.107Z | 330.069° NNW |
7 mins | 2025-08-14 18:02:48.107Z | 42.99° NE | 2025-08-14 18:05:48.107Z | 75.028° E | 17.967° | 2025-08-14 18:09:48.107Z | 116.918° SE |
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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