SHIYAN 27F, 63604
Orbit data source: Space-Track
SHIYAN 27F, 63604 is a payload satellite owned by CAST (CN) in SSO that was launched on Fri, 18 Apr 2025 UTC via a CHANG ZHENG 6A launch vehicle from the Taiyaun Space Center, China (TSC). 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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63604 intel report (Beta)
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Expand to show TLE details & historyLast TLE update: 5 hours ago
TLE from 5 hours ago
0 SHIYAN 27F
1 63604U 25078F 26035.19935788 .00000000 00000-0 62541-4 0 9999
2 63604 99.6935 44.3941 0000738 85.3616 274.7607 13.57236308 39490TLE epoch observation values (Epoch: 2026-02-04T04:47:04.520Z)
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Visualization observer readout
Orbital elements
Other satellites on launch #78 in the year 2025 (2025-04-18 UTC)
SHIYAN 27F 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. |
|---|---|---|---|---|---|---|---|
| 11 mins | 2026-02-04 12:27:56.440Z | 35.897° NE | 2026-02-04 12:32:56.440Z | 88.38° E | 27.393° | 2026-02-04 12:38:56.440Z | 157.219° SSE |
| 10 mins | 2026-02-04 14:13:56.440Z | 352.915° N | 2026-02-04 14:17:56.440Z | 295.947° NW | 33.953° | 2026-02-04 14:23:56.440Z | 225.028° WSW |
| 5 mins | 2026-02-04 22:40:56.440Z | 77.643° E | 2026-02-04 22:42:56.440Z | 57.108° ENE | 14.936° | 2026-02-04 22:45:56.440Z | 27.4° NE |
| 11 mins | 2026-02-05 00:21:56.440Z | 162.681° S | 2026-02-05 00:26:56.440Z | 358.29° N | 44.854° | 2026-02-05 00:32:56.440Z | 345.69° N |
| 4 mins | 2026-02-05 02:10:56.440Z | 259.412° W | 2026-02-05 02:11:56.440Z | 269.401° W | 13.054° | 2026-02-05 02:14:56.440Z | 297.844° NW |
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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