QIANFAN-84, 63170
Orbit data source: Space-Track
QIANFAN-84, 63170 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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63170 intel report (Beta)
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TLE from 14 hours ago
0 QIANFAN-84
1 63170U 25046M 25225.90019694 .00000164 00000-0 23473-3 0 9991
2 63170 88.9864 332.5059 0017852 114.0464 246.2558 13.50967683 31084
TLE epoch observation values (Epoch: 2025-08-13T21:36:17.015Z)
Visualization orbit readout
Visualization observer readout
Orbital elements
Other satellites on launch #46 in the year 2025 (2025-03-11 UTC)
QIANFAN-84 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 | 2025-08-14 17:47:27.808Z | 48.792° ENE | 2025-08-14 17:50:27.808Z | 77.763° E | 13.926° | 2025-08-14 17:53:27.808Z | 105.57° ESE |
11 mins | 2025-08-14 19:32:27.808Z | 358.857° N | 2025-08-14 19:37:27.808Z | 279.842° WNW | 44.825° | 2025-08-14 19:43:27.808Z | 185.935° SSW |
4 mins | 2025-08-15 05:47:27.808Z | 84.576° E | 2025-08-15 05:49:27.808Z | 65.679° ENE | 12.265° | 2025-08-15 05:51:27.808Z | 47.574° ENE |
11 mins | 2025-08-15 07:29:27.808Z | 175.043° S | 2025-08-15 07:34:27.808Z | 101.525° ESE | 44.929° | 2025-08-15 07:40:27.808Z | 0.218° NNE |
4 mins | 2025-08-15 09:20:27.808Z | 271.737° WNW | 2025-08-15 09:21:27.808Z | 281.522° WNW | 13.542° | 2025-08-15 09:24:27.808Z | 310.206° 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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