STARLINK-1712, 46581
Orbit data source: Space-Track
STARLINK-1712, 46581 is a payload satellite owned by SpaceX/Seattle (US) in LEO that was launched on Tue, 06 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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46581 intel report (Beta)
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Expand to show TLE details & historyLast TLE update: 5 hours ago
TLE from 5 hours ago
0 STARLINK-1712
1 46581U 20070BB 25286.66667824 .00032630 00000-0 75342-3 0 9999
2 46581 53.0516 78.3378 0008141 167.7492 245.0581 15.42234946 5945
TLE epoch observation values (Epoch: 2025-10-13T16:00:00.999Z)
Visualization orbit readout
Visualization observer readout
Orbital elements
Other satellites on launch #70 in the year 2020 (2020-10-06 UTC)
STARLINK-1712 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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4 mins | 2025-10-13 20:59:22.519Z | 270.723° WNW | 2025-10-13 21:01:22.519Z | 222.939° SW | 21.099° | 2025-10-13 21:03:22.519Z | 181.48° SSW |
4 mins | 2025-10-14 12:10:22.519Z | 166.786° S | 2025-10-14 12:11:22.519Z | 137.895° SSE | 25.225° | 2025-10-14 12:14:22.519Z | 72.873° E |
4 mins | 2025-10-14 13:47:22.519Z | 287.856° WNW | 2025-10-14 13:48:22.519Z | 319.1° NNW | 28.05° | 2025-10-14 13:51:22.519Z | 31.284° NE |
4 mins | 2025-10-14 18:41:22.519Z | 344.058° N | 2025-10-14 18:43:22.519Z | 38.941° NE | 24.657° | 2025-10-14 18:45:22.519Z | 83.448° E |
5 mins | 2025-10-14 20:18:22.519Z | 281.18° WNW | 2025-10-14 20:20:22.519Z | 221.229° SW | 29.66° | 2025-10-14 20:23:22.519Z | 159.693° S |
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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