STARLINK-1527, 46048
Orbit data source: Space-Track
STARLINK-1527, 46048 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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46048 intel report (Beta)
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Expand to show TLE details & historyLast TLE update: 19 hours ago
TLE from 19 hours ago
0 STARLINK-1527
1 46048U 20055X 25291.28670041 .00001084 00000-0 91647-4 0 9995
2 46048 53.0526 35.8897 0001322 90.5119 269.6022 15.06402721287549
TLE epoch observation values (Epoch: 2025-10-18T06:52:50.915Z)
Visualization orbit readout
Visualization observer readout
Orbital elements
Other satellites on launch #55 in the year 2020 (2020-08-07 UTC)
STARLINK-1527 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 | 2025-10-19 08:30:03.903Z | 174.534° S | 2025-10-19 08:33:03.903Z | 125.838° SE | 18.887° | 2025-10-19 08:35:03.903Z | 90.591° ESE |
6 mins | 2025-10-19 10:10:03.903Z | 254.564° W | 2025-10-19 10:12:03.903Z | 316.925° NNW | 39.83° | 2025-10-19 10:16:03.903Z | 43.251° NE |
4 mins | 2025-10-19 11:51:03.903Z | 320.071° NNW | 2025-10-19 11:52:03.903Z | 337.454° NNW | 16.307° | 2025-10-19 11:55:03.903Z | 25.091° NE |
5 mins | 2025-10-19 15:12:03.903Z | 345.304° N | 2025-10-19 15:14:03.903Z | 30.112° NE | 24.46° | 2025-10-19 15:17:03.903Z | 82.829° E |
6 mins | 2025-10-19 16:51:03.903Z | 296.283° NW | 2025-10-19 16:54:03.903Z | 198.344° SSW | 38.521° | 2025-10-19 16:57:03.903Z | 148.338° 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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