STARLINK-32705, 62479
Orbit data source: Space-Track
STARLINK-32705, 62479 is a payload satellite owned by SpaceX/Seattle (US) in LEO that was launched on Tue, 31 Dec 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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62479 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-32705
1 62479U 24254T 25260.04336908 .00029703 00000-0 10838-2 0 9996
2 62479 43.0012 269.4532 0002723 284.6660 75.3889 15.27602068 41021
TLE epoch observation values (Epoch: 2025-09-17T01:02:27.088Z)
Visualization orbit readout
Visualization observer readout
Orbital elements
Other satellites on launch #254 in the year 2024 (2024-12-31 UTC)
STARLINK-32705 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 | 2025-09-18 05:34:36.320Z | 268.566° W | 2025-09-18 05:37:36.320Z | 359.003° N | 41.767° | 2025-09-18 05:40:36.320Z | 69.237° E |
5 mins | 2025-09-18 07:14:36.320Z | 295.952° NW | 2025-09-18 07:16:36.320Z | 358.256° N | 39.26° | 2025-09-18 07:19:36.320Z | 82.485° E |
5 mins | 2025-09-18 08:53:36.320Z | 278.479° WNW | 2025-09-18 08:55:36.320Z | 216.289° SW | 41.372° | 2025-09-18 08:58:36.320Z | 125.489° SE |
5 mins | 2025-09-19 03:28:36.320Z | 212.074° SW | 2025-09-19 03:30:36.320Z | 159.422° S | 33.048° | 2025-09-19 03:33:36.320Z | 85.03° E |
5 mins | 2025-09-19 05:07:36.320Z | 272.272° WNW | 2025-09-19 05:09:36.320Z | 344.153° N | 42.038° | 2025-09-19 05:12:36.320Z | 68.776° 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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