STARLINK-31956, 59930
Orbit data source: Space-Track
STARLINK-31956, 59930 is a payload satellite owned by SpaceX/Seattle (US) in LEO that was launched on Sat, 01 Jun 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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59930 intel report (Beta)
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Expand to show TLE details & historyLast TLE update: 9 hours ago
TLE from 9 hours ago
0 STARLINK-31956
1 59930U 24106J 25289.12308139 .00001335 00000-0 58038-4 0 9992
2 59930 43.0037 68.9206 0001160 281.8165 78.2557 15.27574656 78417
TLE epoch observation values (Epoch: 2025-10-16T02:57:14.232Z)
Visualization orbit readout
Visualization observer readout
Orbital elements
Other satellites on launch #106 in the year 2024 (2024-06-01 UTC)
STARLINK-31956 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 | 2025-10-16 12:33:48.535Z | 206.42° SW | 2025-10-16 12:36:48.535Z | 144.56° SSE | 26.048° | 2025-10-16 12:39:48.535Z | 88.036° E |
6 mins | 2025-10-16 14:12:48.535Z | 259.389° W | 2025-10-16 14:15:48.535Z | 38.873° NE | 42.846° | 2025-10-16 14:18:48.535Z | 70.562° E |
5 mins | 2025-10-16 15:52:48.535Z | 296.991° NW | 2025-10-16 15:54:48.535Z | 14.061° NNE | 37.898° | 2025-10-16 15:57:48.535Z | 77.896° E |
5 mins | 2025-10-16 17:31:48.535Z | 286.015° WNW | 2025-10-16 17:33:48.535Z | 171.853° S | 44.784° | 2025-10-16 17:36:48.535Z | 112.571° SE |
4 mins | 2025-10-16 19:10:48.535Z | 247.376° WSW | 2025-10-16 19:12:48.535Z | 204.758° SW | 18.742° | 2025-10-16 19:14:48.535Z | 170.33° 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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