STARLINK-6240, 57084
Orbit data source: Space-Track
STARLINK-6240, 57084 is a payload satellite owned by SpaceX/Seattle (US) in LEO that was launched on Thu, 22 Jun 2023 UTC via an FALCON 9 launch vehicle from the Air Force Western Test Range (AFWTR). 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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57084 intel report (Beta)
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Expand to show TLE details & historyLast TLE update: 2 days ago
TLE from 2 days ago
0 STARLINK-6240
1 57084U 23088AN 25254.57028853 -.00000863 00000-0 -48838-4 0 9995
2 57084 43.0055 347.9090 0001415 270.2816 89.7864 15.02529542123577
TLE epoch observation values (Epoch: 2025-09-11T13:41:12.928Z)
Visualization orbit readout
Visualization observer readout
Orbital elements
Other satellites on launch #88 in the year 2023 (2023-06-22 UTC)
STARLINK-6240 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 08:58:00.623Z | 210.849° SW | 2025-09-13 09:01:00.623Z | 148.558° SSE | 30.943° | 2025-09-13 09:04:00.623Z | 87.436° E |
6 mins | 2025-09-13 10:39:00.623Z | 264.23° W | 2025-09-13 10:42:00.623Z | 37.704° NE | 41.935° | 2025-09-13 10:45:00.623Z | 70.3° E |
6 mins | 2025-09-13 12:20:00.623Z | 292.569° NW | 2025-09-13 12:22:00.623Z | 335.777° NNW | 38.603° | 2025-09-13 12:26:00.623Z | 81.764° E |
6 mins | 2025-09-13 14:01:00.623Z | 282.728° WNW | 2025-09-13 14:03:00.623Z | 238.343° WSW | 43.373° | 2025-09-13 14:07:00.623Z | 117.984° SE |
4 mins | 2025-09-13 15:42:00.623Z | 244.414° WSW | 2025-09-13 15:43:00.623Z | 227.018° WSW | 17.73° | 2025-09-13 15:46:00.623Z | 176.974° 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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