STARLINK-34140, 64085
Orbit data source: Space-Track
STARLINK-34140, 64085 is a payload satellite owned by SpaceX/Seattle (US) in LEO that was launched on Wed, 21 May 2025 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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64085 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-34140
1 64085U 25107X 25274.62873392 .00050054 00000-0 18143-2 0 9991
2 64085 43.0021 19.8804 0001177 251.3363 108.7362 15.27614128 21775
TLE epoch observation values (Epoch: 2025-10-01T15:05:22.610Z)
Visualization orbit readout
Visualization observer readout
Orbital elements
Other satellites on launch #107 in the year 2025 (2025-05-21 UTC)
STARLINK-34140 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 | 2025-10-03 09:38:46.898Z | 209.013° SW | 2025-10-03 09:41:46.898Z | 153.328° SSE | 26.202° | 2025-10-03 09:44:46.898Z | 90.158° ESE |
5 mins | 2025-10-03 11:18:46.898Z | 262.065° W | 2025-10-03 11:20:46.898Z | 5.512° NNE | 44.07° | 2025-10-03 11:23:46.898Z | 70.106° E |
5 mins | 2025-10-03 12:57:46.898Z | 294.34° NW | 2025-10-03 12:59:46.898Z | 357.951° N | 38.115° | 2025-10-03 13:02:46.898Z | 76.801° E |
5 mins | 2025-10-03 14:36:46.898Z | 286.152° WNW | 2025-10-03 14:38:46.898Z | 250.872° W | 44.493° | 2025-10-03 14:41:46.898Z | 113.061° SE |
4 mins | 2025-10-03 16:15:46.898Z | 250.59° W | 2025-10-03 16:17:46.898Z | 209.578° SW | 18.803° | 2025-10-03 16:19:46.898Z | 173.142° 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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