STARLINK-1665, 46356
Orbit data source: Space-Track
STARLINK-1665, 46356 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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46356 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-1665
1 46356U 20062AH 25259.22826916 .00002903 00000-0 21369-3 0 9991
2 46356 53.0551 79.8472 0001344 99.8052 260.3089 15.06399162278015
TLE epoch observation values (Epoch: 2025-09-16T05:28:42.455Z)
Visualization orbit readout
Visualization observer readout
Orbital elements
Other satellites on launch #62 in the year 2020 (2020-09-03 UTC)
STARLINK-1665 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 | 2025-09-16 13:35:31.590Z | 156.528° SSE | 2025-09-16 13:37:31.590Z | 125.04° SE | 14.67° | 2025-09-16 13:39:31.590Z | 94.086° ESE |
7 mins | 2025-09-16 15:13:31.590Z | 238.259° WSW | 2025-09-16 15:16:31.590Z | 320.325° NNW | 43.715° | 2025-09-16 15:20:31.590Z | 46.979° ENE |
4 mins | 2025-09-16 16:55:31.590Z | 319.514° NNW | 2025-09-16 16:56:31.590Z | 338.612° N | 18.077° | 2025-09-16 16:59:31.590Z | 26.678° NE |
4 mins | 2025-09-16 20:16:31.590Z | 349.076° N | 2025-09-16 20:18:31.590Z | 31.174° NE | 21.456° | 2025-09-16 20:20:31.590Z | 67.653° E |
6 mins | 2025-09-16 21:55:31.590Z | 303.925° NW | 2025-09-16 21:58:31.590Z | 170.427° S | 42.267° | 2025-09-16 22:01:31.590Z | 138.354° 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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