STARLINK-1817, 46715
Orbit data source: Space-Track
STARLINK-1817, 46715 is a payload satellite owned by SpaceX/Seattle (US) in LEO that was launched on Sun, 18 Oct 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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46715 intel report (Beta)
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Expand to show TLE details & historyLast TLE update: 17 hours ago
TLE from 17 hours ago
0 STARLINK-1817
1 46715U 20073AX 25286.43739173 .00002644 00000-0 19632-3 0 9995
2 46715 53.0538 182.6592 0001374 94.0617 266.0529 15.06405855274938
TLE epoch observation values (Epoch: 2025-10-13T10:29:50.645Z)
Visualization orbit readout
Visualization observer readout
Orbital elements
Other satellites on launch #73 in the year 2020 (2020-10-18 UTC)
STARLINK-1817 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 | 2025-10-14 18:29:55.029Z | 165.298° S | 2025-10-14 18:31:55.029Z | 130.83° SE | 18.45° | 2025-10-14 18:34:55.029Z | 82.259° E |
6 mins | 2025-10-14 20:08:55.029Z | 251.457° W | 2025-10-14 20:10:55.029Z | 299.951° NW | 39.539° | 2025-10-14 20:14:55.029Z | 42.791° NE |
4 mins | 2025-10-14 21:49:55.029Z | 316.166° NNW | 2025-10-14 21:51:55.029Z | 351.611° N | 16.336° | 2025-10-14 21:53:55.029Z | 22.415° NNE |
5 mins | 2025-10-15 01:10:55.029Z | 342.052° N | 2025-10-15 01:12:55.029Z | 23.78° NE | 24.184° | 2025-10-15 01:15:55.029Z | 80.057° E |
6 mins | 2025-10-15 02:49:55.029Z | 298.337° NW | 2025-10-15 02:52:55.029Z | 212.361° SW | 39.903° | 2025-10-15 02:55:55.029Z | 148.353° 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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