STARLINK-1686, 46328
Orbit data source: Space-Track
STARLINK-1686, 46328 is a payload satellite owned by SpaceX/Seattle (US) in LEO that was launched on Thu, 03 Sep 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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46328 intel report (Beta)
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Expand to show TLE details & historyLast TLE update: 7 hours ago
TLE from 7 hours ago
0 STARLINK-1686
1 46328U 20062D 25287.00005787 .00069924 00000-0 42954-2 0 9990
2 46328 53.0540 295.1240 0001768 96.0777 130.6180 15.09451551 5654
TLE epoch observation values (Epoch: 2025-10-14T00:00:04.999Z)
Visualization orbit readout
Visualization observer readout
Orbital elements
Other satellites on launch #62 in the year 2020 (2020-09-03 UTC)
STARLINK-1686 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 09:00:09.621Z | 345.339° N | 2025-10-14 09:02:09.621Z | 27.73° NE | 22.653° | 2025-10-14 09:05:09.621Z | 79.39° E |
6 mins | 2025-10-14 10:39:09.621Z | 299.73° NW | 2025-10-14 10:41:09.621Z | 262.94° W | 40.261° | 2025-10-14 10:45:09.621Z | 142.933° SSE |
4 mins | 2025-10-15 02:11:09.621Z | 157.894° S | 2025-10-15 02:12:09.621Z | 137.638° SSE | 20.495° | 2025-10-15 02:15:09.621Z | 82.551° E |
6 mins | 2025-10-15 03:49:09.621Z | 256.636° W | 2025-10-15 03:51:09.621Z | 301.4° NW | 36.55° | 2025-10-15 03:55:09.621Z | 40.525° NE |
4 mins | 2025-10-15 05:30:09.621Z | 319.291° NNW | 2025-10-15 05:31:09.621Z | 335.898° NNW | 15.242° | 2025-10-15 05:34:09.621Z | 23.811° 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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