STARLINK-1540, 46051
Orbit data source: Space-Track
STARLINK-1540, 46051 is a payload satellite owned by SpaceX/Seattle (US) in LEO that was launched on Fri, 07 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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46051 intel report (Beta)
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Expand to show TLE details & historyLast TLE update: 13 hours ago
TLE from 13 hours ago
0 STARLINK-1540
1 46051U 20055AA 25294.57089041 .00002426 00000-0 18175-3 0 9993
2 46051 53.0554 21.1494 0001622 82.8998 277.2176 15.06396380288074
TLE epoch observation values (Epoch: 2025-10-21T13:42:04.931Z)
Visualization orbit readout
Visualization observer readout
Orbital elements
Other satellites on launch #55 in the year 2020 (2020-08-07 UTC)
STARLINK-1540 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 | 2025-10-22 07:22:27.915Z | 160.795° S | 2025-10-22 07:24:27.915Z | 125.749° SE | 17.607° | 2025-10-22 07:26:27.915Z | 91.773° ESE |
6 mins | 2025-10-22 09:01:27.915Z | 251.164° W | 2025-10-22 09:03:27.915Z | 316.771° NNW | 41.097° | 2025-10-22 09:07:27.915Z | 44.272° NE |
4 mins | 2025-10-22 10:42:27.915Z | 319.803° NNW | 2025-10-22 10:43:27.915Z | 337.624° N | 16.772° | 2025-10-22 10:46:27.915Z | 25.446° NE |
5 mins | 2025-10-22 14:03:27.915Z | 346.36° N | 2025-10-22 14:05:27.915Z | 30.303° NE | 23.544° | 2025-10-22 14:08:27.915Z | 81.351° E |
6 mins | 2025-10-22 15:42:27.915Z | 298.47° NW | 2025-10-22 15:45:27.915Z | 193.168° SSW | 39.903° | 2025-10-22 15:48:27.915Z | 145.489° 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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