STARLINK-5682, 55457
Orbit data source: Space-Track
STARLINK-5682, 55457 is a payload satellite owned by SpaceX/Seattle (US) in LEO that was launched on Thu, 02 Feb 2023 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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55457 intel report (Beta)
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Expand to show TLE details & historyLast TLE update: 12 hours ago
TLE from 12 hours ago
0 STARLINK-5682
1 55457U 23015J 25288.65182163 .00001910 00000-0 15637-3 0 9990
2 55457 43.0034 34.3337 0000690 256.7360 103.3406 15.02548517148939
TLE epoch observation values (Epoch: 2025-10-15T15:38:37.388Z)
Visualization orbit readout
Visualization observer readout
Orbital elements
Other satellites on launch #15 in the year 2023 (2023-02-02 UTC)
STARLINK-5682 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 | 2025-10-16 09:22:31.068Z | 171.817° S | 2025-10-16 09:24:31.068Z | 139.226° SSE | 16.017° | 2025-10-16 09:26:31.068Z | 107.841° ESE |
7 mins | 2025-10-16 11:01:31.068Z | 236.46° WSW | 2025-10-16 11:04:31.068Z | 162.275° S | 42.738° | 2025-10-16 11:08:31.068Z | 74.669° E |
6 mins | 2025-10-16 12:42:31.068Z | 279.397° WNW | 2025-10-16 12:45:31.068Z | 6.638° NNE | 40.04° | 2025-10-16 12:48:31.068Z | 70.808° E |
6 mins | 2025-10-16 14:23:31.068Z | 291.955° WNW | 2025-10-16 14:26:31.068Z | 37.17° NE | 42.692° | 2025-10-16 14:29:31.068Z | 94.634° ESE |
6 mins | 2025-10-16 16:04:31.068Z | 268.701° W | 2025-10-16 16:06:31.068Z | 223.685° SW | 32.919° | 2025-10-16 16:10:31.068Z | 140.475° SSE |
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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