STARLINK-1365, 45590
Orbit data source: Space-Track
STARLINK-1365, 45590 is a payload satellite owned by SpaceX/Seattle (US) in LEO that was launched on Wed, 22 Apr 2020 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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45590 intel report (Beta)
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Expand to show TLE details & historyLast TLE update: 1 day ago
TLE from 1 day ago
0 STARLINK-1365
1 45590U 20025BM 25288.60426303 .00001907 00000-0 14692-3 0 9993
2 45590 53.0554 37.9292 0001239 75.4380 284.6747 15.06396533303231
TLE epoch observation values (Epoch: 2025-10-15T14:30:08.325Z)
Visualization orbit readout
Visualization observer readout
Orbital elements
Other satellites on launch #25 in the year 2020 (2020-04-22 UTC)
STARLINK-1365 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 14:48:28.893Z | 334.808° NNW | 2025-10-16 14:51:28.893Z | 22.535° NE | 16.493° | 2025-10-16 14:53:28.893Z | 54.265° ENE |
6 mins | 2025-10-16 16:28:28.893Z | 320.249° NNW | 2025-10-16 16:31:28.893Z | 43.326° NE | 40.345° | 2025-10-16 16:34:28.893Z | 113.158° SE |
4 mins | 2025-10-16 18:09:28.893Z | 253.462° W | 2025-10-16 18:10:28.893Z | 234.153° WSW | 18.377° | 2025-10-16 18:13:28.893Z | 186.241° SSW |
7 mins | 2025-10-17 09:40:28.893Z | 223.534° SW | 2025-10-17 09:43:28.893Z | 153.754° SSE | 44.437° | 2025-10-17 09:47:28.893Z | 52.526° ENE |
5 mins | 2025-10-17 11:21:28.893Z | 298.45° NW | 2025-10-17 11:23:28.893Z | 337.52° N | 21.038° | 2025-10-17 11:26:28.893Z | 27.86° NE |
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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