STARLINK-32468, 62149
Orbit data source: Space-Track
STARLINK-32468, 62149 is a payload satellite owned by SpaceX/Seattle (US) in LEO that was launched on Sat, 30 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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62149 intel report (Beta)
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TLE from 12 hours ago
0 STARLINK-32468
1 62149U 24224L 25218.91597134 .00016573 00000-0 61042-3 0 9991
2 62149 43.0003 290.9925 0001285 266.9507 93.1198 15.27580317 39474
TLE epoch observation values (Epoch: 2025-08-06T21:58:59.923Z)
Visualization orbit readout
Visualization observer readout
Orbital elements
Other satellites on launch #224 in the year 2024 (2024-11-30 UTC)
STARLINK-32468 Visibility forecast
Observer location: undefined°, undefined°
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 | 2025-08-07 10:52:16.399Z | 283.703° WNW | 2025-08-07 10:55:16.399Z | 6.194° NNE | 38.029° | 2025-08-07 10:58:16.399Z | 73.231° E |
5 mins | 2025-08-07 12:32:16.399Z | 292.407° WNW | 2025-08-07 12:34:16.399Z | 3.646° NNE | 44.223° | 2025-08-07 12:37:16.399Z | 101.309° ESE |
5 mins | 2025-08-07 14:11:16.399Z | 257.067° W | 2025-08-07 14:13:16.399Z | 205.594° SW | 25.925° | 2025-08-07 14:16:16.399Z | 151.102° SSE |
4 mins | 2025-08-08 07:08:16.399Z | 173.575° S | 2025-08-08 07:09:16.399Z | 153.471° SSE | 18.411° | 2025-08-08 07:12:16.399Z | 98.335° ESE |
5 mins | 2025-08-08 08:46:16.399Z | 245.289° WSW | 2025-08-08 08:48:16.399Z | 155.766° SSE | 44.741° | 2025-08-08 08:51:16.399Z | 73.161° 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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Event ID | Pc | Md | Secondary | Secondary name | Country | Click to unsort rows by TCA header |
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