STARLINK-1718, 46674
Orbit data source: Space-Track
STARLINK-1718, 46674 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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46674 intel report (Beta)
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Expand to show TLE details & historyLast TLE update: 18 hours ago
TLE from 18 hours ago
0 STARLINK-1718
1 46674U 20073E 25287.95232449 .00001455 00000-0 11662-3 0 9995
2 46674 53.0522 175.8607 0001610 80.9443 279.1728 15.06387548275160
TLE epoch observation values (Epoch: 2025-10-14T22:51:20.835Z)
Visualization orbit readout
Visualization observer readout
Orbital elements
Other satellites on launch #73 in the year 2020 (2020-10-18 UTC)
STARLINK-1718 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 | 2025-10-15 18:07:06.658Z | 164.29° S | 2025-10-15 18:09:06.658Z | 130.092° SE | 18.03° | 2025-10-15 18:12:06.658Z | 82.341° E |
6 mins | 2025-10-15 19:46:06.658Z | 250.62° W | 2025-10-15 19:48:06.658Z | 301.006° NW | 40.091° | 2025-10-15 19:52:06.658Z | 43.269° NE |
4 mins | 2025-10-15 21:27:06.658Z | 316.476° NNW | 2025-10-15 21:29:06.658Z | 352.275° N | 16.423° | 2025-10-15 21:31:06.658Z | 22.884° NE |
5 mins | 2025-10-16 00:48:06.658Z | 342.735° N | 2025-10-16 00:50:06.658Z | 24.592° NE | 23.915° | 2025-10-16 00:53:06.658Z | 79.836° E |
6 mins | 2025-10-16 02:27:06.658Z | 298.851° NW | 2025-10-16 02:30:06.658Z | 209.644° SW | 40.32° | 2025-10-16 02:33:06.658Z | 147.287° 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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