STARLINK-4672, 53592
Orbit data source: Space-Track
STARLINK-4672, 53592 is a payload satellite owned by SpaceX/Seattle (US) in LEO that was launched on Sun, 28 Aug 2022 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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53592 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-4672
1 53592U 22104E 25286.70825222 -.00000621 00000-0 -20924-4 0 9996
2 53592 53.2154 184.0894 0001499 82.7375 277.3787 15.08825613173758
TLE epoch observation values (Epoch: 2025-10-13T16:59:52.991Z)
Visualization orbit readout
Visualization observer readout
Orbital elements
Other satellites on launch #104 in the year 2022 (2022-08-28 UTC)
STARLINK-4672 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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7 mins | 2025-10-14 20:12:40.720Z | 241.965° WSW | 2025-10-14 20:16:40.720Z | 353.257° N | 40.492° | 2025-10-14 20:19:40.720Z | 42.792° NE |
4 mins | 2025-10-14 21:54:40.720Z | 313.593° NW | 2025-10-14 21:56:40.720Z | 349.297° N | 16.473° | 2025-10-14 21:58:40.720Z | 20.855° NNE |
5 mins | 2025-10-15 01:15:40.720Z | 346.65° N | 2025-10-15 01:17:40.720Z | 28.824° NE | 22.251° | 2025-10-15 01:20:40.720Z | 79.244° E |
6 mins | 2025-10-15 02:54:40.720Z | 300.763° NW | 2025-10-15 02:56:40.720Z | 265.319° W | 40.652° | 2025-10-15 03:00:40.720Z | 142.299° SSE |
5 mins | 2025-10-15 18:26:40.720Z | 165.949° S | 2025-10-15 18:28:40.720Z | 125.67° SE | 21.125° | 2025-10-15 18:31:40.720Z | 76.916° E |
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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