GUANGCHUAN 01, 62111
Orbit data source: Space-Track
GUANGCHUAN 01, 62111 is a Chinese payload satellite in LEO that was launched on Wed, 27 Nov 2024 UTC via a ZHUQUE-2E launch vehicle from the Jiuquan Satellite Launch Center, China (JSC). 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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62111 intel report (Beta)
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Expand to show TLE details & historyLast TLE update: 6 hours ago
TLE from 6 hours ago
0 GUANGCHUAN 01
1 62111U 24221A 25256.98614897 .00002747 00000-0 16336-3 0 9996
2 62111 49.9447 68.0982 0007598 261.5403 98.4687 15.14489610 44305
TLE epoch observation values (Epoch: 2025-09-13T23:40:03.271Z)
Visualization orbit readout
Visualization observer readout
Orbital elements
Other satellites on launch #221 in the year 2024 (2024-11-27 UTC)
GUANGCHUAN 01 Visibility forecast
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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 | 2025-09-14 14:05:43.824Z | 209.333° SW | 2025-09-14 14:08:43.824Z | 139.561° SSE | 36.074° | 2025-09-14 14:11:43.824Z | 69.829° E |
6 mins | 2025-09-14 15:45:43.824Z | 280.766° WNW | 2025-09-14 15:47:43.824Z | 324.744° NNW | 29.448° | 2025-09-14 15:51:43.824Z | 44.186° NE |
4 mins | 2025-09-14 17:26:43.824Z | 329.202° NNW | 2025-09-14 17:27:43.824Z | 347.837° N | 18.036° | 2025-09-14 17:30:43.824Z | 40.382° NE |
5 mins | 2025-09-14 19:06:43.824Z | 339.07° N | 2025-09-14 19:08:43.824Z | 26.737° NE | 24.038° | 2025-09-14 19:11:43.824Z | 76.205° E |
6 mins | 2025-09-14 20:45:43.824Z | 300.44° NW | 2025-09-14 20:47:43.824Z | 267.737° W | 43.988° | 2025-09-14 20:51:43.824Z | 129.428° 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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