STARLINK-5362, 55493
Orbit data source: Space-Track
STARLINK-5362, 55493 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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55493 intel report (Beta)
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Expand to show TLE details & historyLast TLE update: 9 hours ago
TLE from 9 hours ago
0 STARLINK-5362
1 55493U 23015AW 25288.62494021 .00000714 00000-0 67948-4 0 9990
2 55493 43.0047 47.1155 0001192 271.8591 88.2115 15.02536904148783
TLE epoch observation values (Epoch: 2025-10-15T14:59:54.834Z)
Visualization orbit readout
Visualization observer readout
Orbital elements
Other satellites on launch #15 in the year 2023 (2023-02-02 UTC)
STARLINK-5362 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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5 mins | 2025-10-16 10:19:11.809Z | 183.23° SSW | 2025-10-16 10:22:11.809Z | 133.734° SE | 17.623° | 2025-10-16 10:24:11.809Z | 102.741° ESE |
6 mins | 2025-10-16 11:59:11.809Z | 239.907° WSW | 2025-10-16 12:02:11.809Z | 126.316° SE | 43.441° | 2025-10-16 12:05:11.809Z | 74.856° E |
6 mins | 2025-10-16 13:40:11.809Z | 283.017° WNW | 2025-10-16 13:43:11.809Z | 22.442° NNE | 38.79° | 2025-10-16 13:46:11.809Z | 72.698° E |
6 mins | 2025-10-16 15:21:11.809Z | 292.353° WNW | 2025-10-16 15:24:11.809Z | 64.41° ENE | 41.985° | 2025-10-16 15:27:11.809Z | 98.15° ESE |
5 mins | 2025-10-16 17:02:11.809Z | 262.77° W | 2025-10-16 17:04:11.809Z | 212.618° SW | 31.115° | 2025-10-16 17:07:11.809Z | 149.108° 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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