KORSAT-1, 59452
Orbit data source: Space-Track
KORSAT-1, 59452 is a payload satellite owned by DAPA (KR) in LEO that was launched on Sun, 07 Apr 2024 UTC via an FALCON 9 launch vehicle from the Air Force Eastern Test Range (AFETR). 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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59452 intel report (Beta)
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Expand to show TLE details & historyLast TLE update: 21 hours ago
TLE from 21 hours ago
0 KORSAT-1
1 59452U 24066L 25293.70595959 .00008805 00000-0 73838-3 0 9996
2 59452 45.4117 46.0474 0009116 179.9395 180.1486 14.98741792 84129
TLE epoch observation values (Epoch: 2025-10-20T16:56:34.908Z)
Visualization orbit readout
Visualization observer readout
Orbital elements
Other satellites on launch #66 in the year 2024 (2024-04-07 UTC)
KORSAT-1 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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4 mins | 2025-10-21 14:09:15.997Z | 350.911° N | 2025-10-21 14:09:15.997Z | 350.911° N | 32.017° | 2025-10-21 14:13:15.997Z | 73.047° E |
6 mins | 2025-10-21 15:48:15.997Z | 298.288° NW | 2025-10-21 15:50:15.997Z | 320.858° NNW | 42.949° | 2025-10-21 15:54:15.997Z | 110.02° ESE |
5 mins | 2025-10-21 17:29:15.997Z | 256.417° W | 2025-10-21 17:31:15.997Z | 216.375° SW | 22.21° | 2025-10-21 17:34:15.997Z | 167.549° S |
7 mins | 2025-10-22 10:45:15.997Z | 234.786° WSW | 2025-10-22 10:48:15.997Z | 181.051° SSW | 43.464° | 2025-10-22 10:52:15.997Z | 68.414° E |
6 mins | 2025-10-22 12:27:15.997Z | 291.175° WNW | 2025-10-22 12:29:15.997Z | 343.36° N | 34.545° | 2025-10-22 12:33:15.997Z | 62.087° 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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