YUNHAI 2-1D, 43912
Orbit data source: Space-Track
YUNHAI 2-1D, 43912 is a payload satellite owned by CASC (CN) in LEO that was launched on Sat, 29 Dec 2018 UTC via a CHANG ZHENG 2D/YZ-3 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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43912 intel report (Beta)
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Expand to show TLE details & historyLast TLE update: 6 hours ago
TLE from 6 hours ago
0 YUNHAI 2-1D
1 43912U 18112D 25258.35590880 .00000204 00000-0 14383-3 0 9990
2 43912 50.0121 13.9300 0015645 100.6068 259.6611 14.28853428348288
TLE epoch observation values (Epoch: 2025-09-15T08:32:30.52Z)
Visualization orbit readout
Visualization observer readout
Orbital elements
Other satellites on launch #112 in the year 2018 (2018-12-29 UTC)
YUNHAI 2-1D 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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9 mins | 2025-09-15 15:40:45.350Z | 311.808° NW | 2025-09-15 15:45:45.350Z | 25.661° NE | 31.718° | 2025-09-15 15:49:45.350Z | 83.363° E |
8 mins | 2025-09-15 17:27:45.350Z | 297.869° NW | 2025-09-15 17:30:45.350Z | 257.523° W | 42.577° | 2025-09-15 17:35:45.350Z | 136.11° SSE |
8 mins | 2025-09-16 09:52:45.350Z | 199.764° SSW | 2025-09-16 09:56:45.350Z | 133.891° SE | 33.64° | 2025-09-16 10:00:45.350Z | 71.552° E |
9 mins | 2025-09-16 11:37:45.350Z | 260.37° W | 2025-09-16 11:41:45.350Z | 321.557° NNW | 38.231° | 2025-09-16 11:46:45.350Z | 48.948° ENE |
8 mins | 2025-09-16 13:24:45.350Z | 302.715° NW | 2025-09-16 13:28:45.350Z | 2.332° NNE | 25.416° | 2025-09-16 13:32:45.350Z | 52.703° ENE |
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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