STARLINK-1597, 46142
Orbit data source: Space-Track
STARLINK-1597, 46142 is a payload satellite owned by SpaceX/Seattle (US) in LEO that was launched on Tue, 18 Aug 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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46142 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-1597
1 46142U 20057AB 25260.54597558 -.00000014 00000-0 17964-4 0 9991
2 46142 53.0567 13.8927 0001142 95.9521 264.1599 15.06382556279964
TLE epoch observation values (Epoch: 2025-09-17T13:06:12.29Z)
Visualization orbit readout
Visualization observer readout
Orbital elements
Other satellites on launch #57 in the year 2020 (2020-08-18 UTC)
STARLINK-1597 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 | 2025-09-18 18:19:14.659Z | 278.645° WNW | 2025-09-18 18:22:14.659Z | 230.196° WSW | 18.851° | 2025-09-18 18:24:14.659Z | 194.869° SSW |
6 mins | 2025-09-19 09:52:14.659Z | 222.097° SW | 2025-09-19 09:55:14.659Z | 116.641° SE | 44.134° | 2025-09-19 09:58:14.659Z | 53.946° ENE |
5 mins | 2025-09-19 11:33:14.659Z | 300.743° NW | 2025-09-19 11:35:14.659Z | 341.677° N | 21.217° | 2025-09-19 11:38:14.659Z | 29.696° NE |
4 mins | 2025-09-19 14:55:14.659Z | 353.836° N | 2025-09-19 14:56:14.659Z | 12.353° NNE | 18.159° | 2025-09-19 14:59:14.659Z | 63.181° ENE |
6 mins | 2025-09-19 16:34:14.659Z | 315.762° NNW | 2025-09-19 16:36:14.659Z | 344.79° N | 42.448° | 2025-09-19 16:40:14.659Z | 124.163° SE |
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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