STARLINK-1807, 46706
Orbit data source: Space-Track
STARLINK-1807, 46706 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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46706 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-1807
1 46706U 20073AN 25255.90544427 .00017469 00000-0 10924-2 0 9994
2 46706 53.0517 319.1252 0004590 319.1552 40.9094 15.09517616270346
TLE epoch observation values (Epoch: 2025-09-12T21:43:50.384Z)
Visualization orbit readout
Visualization observer readout
Orbital elements
Other satellites on launch #73 in the year 2020 (2020-10-18 UTC)
STARLINK-1807 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 | 2025-09-14 05:39:48.533Z | 170.465° S | 2025-09-14 05:41:48.533Z | 136.601° SSE | 19.248° | 2025-09-14 05:44:48.533Z | 83.609° E |
6 mins | 2025-09-14 07:18:48.533Z | 254.04° W | 2025-09-14 07:20:48.533Z | 300.075° NW | 37.94° | 2025-09-14 07:24:48.533Z | 41.614° NE |
4 mins | 2025-09-14 08:59:48.533Z | 319.144° NNW | 2025-09-14 09:00:48.533Z | 336.137° NNW | 15.744° | 2025-09-14 09:03:48.533Z | 24.19° NE |
5 mins | 2025-09-14 12:20:48.533Z | 350.838° N | 2025-09-14 12:22:48.533Z | 39.67° NE | 24.201° | 2025-09-14 12:25:48.533Z | 86.564° E |
5 mins | 2025-09-14 13:59:48.533Z | 290.632° WNW | 2025-09-14 14:01:48.533Z | 225.821° WSW | 38.831° | 2025-09-14 14:04:48.533Z | 151.426° 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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