HONGYUN 1, 43871
Orbit data source: Space-Track
HONGYUN 1, 43871 is a payload satellite owned by CASIC (CN) in SSO that was launched on Fri, 21 Dec 2018 UTC via a CHANG ZHENG 11 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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43871 intel report (Beta)
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Expand to show TLE details & historyLast TLE update: 5 hours ago
TLE from 5 hours ago
0 HONGYUN 1
1 43871U 18108A 25290.75833154 .00000020 00000-0 99974-4 0 9999
2 43871 99.7898 311.7896 0010739 259.7520 100.2404 13.50754561336358
TLE epoch observation values (Epoch: 2025-10-17T18:11:59.845Z)
Visualization orbit readout
Visualization observer readout
Orbital elements
Other satellites on launch #108 in the year 2018 (2018-12-21 UTC)
HONGYUN 1 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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7 mins | 2025-10-17 23:43:04.547Z | 89.389° E | 2025-10-17 23:46:04.547Z | 60.37° ENE | 16.116° | 2025-10-17 23:50:04.547Z | 21.488° NNE |
12 mins | 2025-10-18 01:25:04.547Z | 164.781° S | 2025-10-18 01:31:04.547Z | 329.965° NNW | 44.481° | 2025-10-18 01:37:04.547Z | 344.596° N |
4 mins | 2025-10-18 03:15:04.547Z | 257.281° W | 2025-10-18 03:16:04.547Z | 266.78° W | 12.472° | 2025-10-18 03:19:04.547Z | 294.708° NW |
11 mins | 2025-10-18 14:22:04.547Z | 19.146° NNE | 2025-10-18 14:27:04.547Z | 143.474° SSE | 44.23° | 2025-10-18 14:33:04.547Z | 191.751° SSW |
7 mins | 2025-10-18 16:08:04.547Z | 333.157° NNW | 2025-10-18 16:11:04.547Z | 301.745° NW | 17.665° | 2025-10-18 16:15:04.547Z | 262.773° W |
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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