STARLINK-32466, 61859
Orbit data source: Space-Track
STARLINK-32466, 61859 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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61859 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-32466
1 61859U 24202Q 25261.04435156 -.00001595 00000-0 -48446-4 0 9995
2 61859 43.0036 133.0100 0001916 284.4058 75.6581 15.27564747 48937
TLE epoch observation values (Epoch: 2025-09-18T01:03:51.974Z)
Visualization orbit readout
Visualization observer readout
Orbital elements
Other satellites on launch #202 in the year 2024 (2024-11-07 UTC)
STARLINK-32466 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 | 2025-09-19 18:03:22.573Z | 205.871° SW | 2025-09-19 18:06:22.573Z | 147.267° SSE | 25.275° | 2025-09-19 18:09:22.573Z | 89.403° E |
6 mins | 2025-09-19 19:42:22.573Z | 257.974° W | 2025-09-19 19:45:22.573Z | 35.64° NE | 43.584° | 2025-09-19 19:48:22.573Z | 70.611° E |
5 mins | 2025-09-19 21:22:22.573Z | 295.697° NW | 2025-09-19 21:24:22.573Z | 8.476° NNE | 38.011° | 2025-09-19 21:27:22.573Z | 76.95° E |
5 mins | 2025-09-19 23:01:22.573Z | 286.981° WNW | 2025-09-19 23:03:22.573Z | 217.393° SW | 44.928° | 2025-09-19 23:06:22.573Z | 111.312° ESE |
4 mins | 2025-09-20 00:40:22.573Z | 249.592° W | 2025-09-20 00:42:22.573Z | 206.536° SW | 19.612° | 2025-09-20 00:44:22.573Z | 170.329° S |
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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