KORSAT-3, 63630
Orbit data source: Space-Track
KORSAT-3, 63630 is a payload satellite owned by DAPA (KR) in LEO that was launched on Tue, 22 Apr 2025 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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63630 intel report (Beta)
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Expand to show TLE details & historyLast TLE update: 16 hours ago
TLE from 16 hours ago
0 KORSAT-3
1 63630U 25081A 25256.61303131 .00006576 00000-0 55625-3 0 9992
2 63630 45.4126 329.9283 0008335 181.5033 178.5822 14.98754505 21686
TLE epoch observation values (Epoch: 2025-09-13T14:42:45.905Z)
Visualization orbit readout
Visualization observer readout
Orbital elements
Other satellites on launch #81 in the year 2025 (2025-04-22 UTC)
KORSAT-3 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 | 2025-09-14 06:52:25.921Z | 170.373° S | 2025-09-14 06:54:25.921Z | 141.174° SSE | 14.967° | 2025-09-14 06:56:25.921Z | 109.822° ESE |
6 mins | 2025-09-14 08:32:25.921Z | 232.853° WSW | 2025-09-14 08:34:25.921Z | 202.959° SW | 42.145° | 2025-09-14 08:38:25.921Z | 68.808° E |
6 mins | 2025-09-14 10:13:25.921Z | 288.233° WNW | 2025-09-14 10:15:25.921Z | 332.506° NNW | 33.904° | 2025-09-14 10:19:25.921Z | 60.722° ENE |
6 mins | 2025-09-14 11:54:25.921Z | 305.354° NW | 2025-09-14 11:57:25.921Z | 22.404° NNE | 33.92° | 2025-09-14 12:00:25.921Z | 78.11° E |
6 mins | 2025-09-14 13:35:25.921Z | 290.164° WNW | 2025-09-14 13:38:25.921Z | 159.532° S | 43.147° | 2025-09-14 13:41:25.921Z | 123.436° SE |
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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