HULIANWANG DIGUI-04, 62326
Orbit data source: Space-Track
HULIANWANG DIGUI-04, 62326 is a payload satellite owned by Zhongguo Xingwang (CN) in LEO that was launched on Mon, 16 Dec 2024 UTC via a CHANG ZHENG 5B/YZ-2 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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62326 intel report (Beta)
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Expand to show TLE details & historyLast TLE update: 15 hours ago
TLE from 15 hours ago
0 HULIANWANG DIGUI-04
1 62326U 24240D 25341.24219462 .00000079 00000-0 15077-3 0 9995
2 62326 86.4984 47.9463 0001664 92.4308 267.7016 13.24414100 47231TLE epoch observation values (Epoch: 2025-12-07T05:48:45.615Z)
Visualization orbit readout
Visualization observer readout
Orbital elements
Other satellites on launch #240 in the year 2024 (2024-12-16 UTC)
HULIANWANG DIGUI-04 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. |
|---|---|---|---|---|---|---|---|
| 9 mins | 2025-12-08 03:41:56.594Z | 121.637° SE | 2025-12-08 03:46:56.594Z | 75.371° E | 20.017° | 2025-12-08 03:50:56.594Z | 37.065° NE |
| 12 mins | 2025-12-08 05:29:56.594Z | 197.012° SSW | 2025-12-08 05:34:56.594Z | 265.724° W | 42.091° | 2025-12-08 05:41:56.594Z | 356.122° N |
| 7 mins | 2025-12-08 15:04:56.594Z | 40.741° NE | 2025-12-08 15:07:56.594Z | 68.839° E | 16.906° | 2025-12-08 15:11:56.594Z | 106.193° ESE |
| 13 mins | 2025-12-08 16:51:56.594Z | 353.938° N | 2025-12-08 16:57:56.594Z | 277.744° WNW | 44.296° | 2025-12-08 17:04:56.594Z | 185.993° SSW |
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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