STARLINK-32486, 61854
Orbit data source: Space-Track
STARLINK-32486, 61854 is a payload satellite owned by SpaceX/Seattle (US) in LEO that was launched on Thu, 07 Nov 2024 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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61854 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-32486
1 61854U 24202K 25255.73005912 -.00001094 00000-0 -30245-4 0 9994
2 61854 43.0031 162.7858 0001072 287.7608 72.3126 15.27575045 48129
TLE epoch observation values (Epoch: 2025-09-12T17:31:17.107Z)
Visualization orbit readout
Visualization observer readout
Orbital elements
Other satellites on launch #202 in the year 2024 (2024-11-07 UTC)
STARLINK-32486 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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6 mins | 2025-09-13 22:01:21.560Z | 250.004° W | 2025-09-13 22:04:21.560Z | 96.742° ESE | 44.946° | 2025-09-13 22:07:21.560Z | 72.103° E |
5 mins | 2025-09-13 23:41:21.560Z | 290.936° WNW | 2025-09-13 23:43:21.560Z | 354.045° N | 37.993° | 2025-09-13 23:46:21.560Z | 73.01° E |
5 mins | 2025-09-14 01:20:21.560Z | 290.844° WNW | 2025-09-14 01:22:21.560Z | 323.51° NNW | 43.968° | 2025-09-14 01:25:21.560Z | 103.362° ESE |
5 mins | 2025-09-14 02:59:21.560Z | 258.077° W | 2025-09-14 03:01:21.560Z | 211.467° SW | 24.453° | 2025-09-14 03:04:21.560Z | 155.04° SSE |
4 mins | 2025-09-14 19:56:21.560Z | 179.043° S | 2025-09-14 19:58:21.560Z | 135.095° SSE | 19.756° | 2025-09-14 20:00:21.560Z | 99.365° ESE |
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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