HULIANWANG DIGUI-22, 63689
Orbit data source: Space-Track
HULIANWANG DIGUI-22, 63689 is a payload satellite owned by Zhongguo Xingwang (CN) in LEO that was launched on Mon, 28 Apr 2025 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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63689 intel report (Beta)
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Expand to show TLE details & historyLast TLE update: 10 hours ago
TLE from 10 hours ago
0 HULIANWANG DIGUI-22
1 63689U 25086C 26171.43952672 .00000025 00000-0 24638-4 0 9992
2 63689 86.5045 311.9620 0001509 110.6476 249.4820 13.24409438 55292TLE epoch observation values (Epoch: 2026-06-20T10:32:55.108Z)
Visualization orbit readout
Visualization observer readout
Orbital elements
Other satellites on launch #86 in the year 2025 (2025-04-28 UTC)
HULIANWANG DIGUI-22 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. |
|---|---|---|---|---|---|---|---|
| 12 mins | 2026-06-20 22:02:19.419Z | 346.427° N | 2026-06-20 22:08:19.419Z | 258.58° W | 39.902° | 2026-06-20 22:14:19.419Z | 197.904° SSW |
| 8 mins | 2026-06-21 08:27:19.419Z | 112.505° SE | 2026-06-21 08:31:19.419Z | 72.951° E | 19.282° | 2026-06-21 08:35:19.419Z | 36.105° NE |
| 13 mins | 2026-06-21 10:13:19.419Z | 193.594° SSW | 2026-06-21 10:19:19.419Z | 275.917° WNW | 42.701° | 2026-06-21 10:26:19.419Z | 357.137° N |
| 7 mins | 2026-06-21 19:49:19.419Z | 42.934° NE | 2026-06-21 19:52:19.419Z | 71.079° E | 16.289° | 2026-06-21 19:56:19.419Z | 107.073° ESE |
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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