STARLINK-31812, 59800
Orbit data source: Space-Track
STARLINK-31812, 59800 is a payload satellite owned by SpaceX/Seattle (US) in LEO that was launched on Sat, 18 May 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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59800 intel report (Beta)
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Expand to show TLE details & historyLast TLE update: 22 hours ago
TLE from 22 hours ago
0 STARLINK-31812
1 59800U 24093U 25291.73090371 .00000139 00000-0 14559-4 0 9990
2 59800 43.0029 290.6952 0000597 259.2183 100.8602 15.27568854 81058
TLE epoch observation values (Epoch: 2025-10-18T17:32:30.080Z)
Visualization orbit readout
Visualization observer readout
Orbital elements
Other satellites on launch #93 in the year 2024 (2024-05-18 UTC)
STARLINK-31812 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 | 2025-10-20 02:41:15.904Z | 204.89° SW | 2025-10-20 02:44:15.904Z | 144.883° SSE | 25.05° | 2025-10-20 02:47:15.904Z | 88.907° E |
6 mins | 2025-10-20 04:20:15.904Z | 257.83° W | 2025-10-20 04:23:15.904Z | 43.359° NE | 43.079° | 2025-10-20 04:26:15.904Z | 70.762° E |
5 mins | 2025-10-20 06:00:15.904Z | 296.6° NW | 2025-10-20 06:02:15.904Z | 13.761° NNE | 37.806° | 2025-10-20 06:05:15.904Z | 77.236° E |
5 mins | 2025-10-20 07:39:15.904Z | 287.099° WNW | 2025-10-20 07:41:15.904Z | 156.768° SSE | 44.911° | 2025-10-20 07:44:15.904Z | 110.99° ESE |
4 mins | 2025-10-20 09:18:15.904Z | 248.357° W | 2025-10-20 09:20:15.904Z | 204.467° SW | 19.615° | 2025-10-20 09:22:15.904Z | 169.041° 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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