STARLINK-5210, 54082
Orbit data source: Space-Track
STARLINK-5210, 54082 is a payload satellite owned by SpaceX/Seattle (US) in LEO that was launched on Thu, 20 Oct 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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54082 intel report (Beta)
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Expand to show TLE details & historyLast TLE update: 20 hours ago
TLE from 20 hours ago
0 STARLINK-5210
1 54082U 22136AH 25260.68506694 .00000106 00000-0 24806-4 0 9993
2 54082 53.2191 30.9519 0002512 96.1344 263.9935 15.08839456160863
TLE epoch observation values (Epoch: 2025-09-17T16:26:29.783Z)
Visualization orbit readout
Visualization observer readout
Orbital elements
Other satellites on launch #136 in the year 2022 (2022-10-20 UTC)
STARLINK-5210 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 13:23:20.276Z | 302.289° NW | 2025-09-18 13:25:20.276Z | 335.838° NNW | 17.554° | 2025-09-18 13:28:20.276Z | 24.883° NE |
4 mins | 2025-09-18 16:45:20.276Z | 352.996° N | 2025-09-18 16:46:20.276Z | 12.841° NNE | 20.345° | 2025-09-18 16:49:20.276Z | 69.223° E |
6 mins | 2025-09-18 18:24:20.276Z | 304.81° NW | 2025-09-18 18:26:20.276Z | 258.022° W | 44.025° | 2025-09-18 18:30:20.276Z | 136.392° SSE |
4 mins | 2025-09-19 09:56:20.276Z | 157.814° S | 2025-09-19 09:58:20.276Z | 119.7° SE | 18.209° | 2025-09-19 10:00:20.276Z | 86.903° E |
6 mins | 2025-09-19 11:34:20.276Z | 249.886° W | 2025-09-19 11:37:20.276Z | 348.839° N | 38.958° | 2025-09-19 11:40:20.276Z | 41.166° NE |
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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