HULIANWANG DIGUI-26, 63693
Orbit data source: Space-Track
HULIANWANG DIGUI-26, 63693 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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63693 intel report (Beta)
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Expand to show TLE details & historyLast TLE update: 7 hours ago
TLE from 7 hours ago
0 HULIANWANG DIGUI-26
1 63693U 25086G 26229.24151459 .00000027 00000-0 28508-4 0 9996
2 63693 86.5067 292.6625 0002591 95.2026 264.9403 13.24411094 62942TLE epoch observation values (Epoch: 2026-08-17T05:47:46.860Z)
Visualization orbit readout
Visualization observer readout
Orbital elements
Other satellites on launch #86 in the year 2025 (2025-04-28 UTC)
HULIANWANG DIGUI-26 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 | 2026-08-17 15:27:53.501Z | 18.453° NNE | 2026-08-17 15:33:53.501Z | 83.606° E | 29.014° | 2026-08-17 15:39:53.501Z | 141.57° SSE |
| 11 mins | 2026-08-17 17:17:53.501Z | 336.087° NNW | 2026-08-17 17:22:53.501Z | 271.471° WNW | 33.382° | 2026-08-17 17:28:53.501Z | 210.418° SW |
| 10 mins | 2026-08-18 03:40:53.501Z | 129.854° SE | 2026-08-18 03:45:53.501Z | 76.048° E | 25.696° | 2026-08-18 03:50:53.501Z | 26.987° NE |
| 12 mins | 2026-08-18 05:28:53.501Z | 208.982° SW | 2026-08-18 05:33:53.501Z | 267.972° W | 36.602° | 2026-08-18 05:40:53.501Z | 350.749° N |
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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