STARLINK-1799, 46699
Orbit data source: Space-Track
STARLINK-1799, 46699 is a payload satellite owned by SpaceX/Seattle (US) in LEO that was launched on Sun, 18 Oct 2020 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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46699 intel report (Beta)
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Expand to show TLE details & historyLast TLE update: 14 hours ago
TLE from 14 hours ago
0 STARLINK-1799
1 46699U 20073AF 25261.08919776 -.00001043 00000-0 -51187-4 0 9995
2 46699 53.0544 296.4515 0001086 78.9663 281.1448 15.06387290271114
TLE epoch observation values (Epoch: 2025-09-18T02:08:26.686Z)
Visualization orbit readout
Visualization observer readout
Orbital elements
Other satellites on launch #73 in the year 2020 (2020-10-18 UTC)
STARLINK-1799 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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4 mins | 2025-09-19 03:46:12.599Z | 163.327° S | 2025-09-19 03:48:12.599Z | 130.619° SE | 16.972° | 2025-09-19 03:50:12.599Z | 95.806° ESE |
6 mins | 2025-09-19 05:25:12.599Z | 247.573° W | 2025-09-19 05:27:12.599Z | 295.382° NW | 40.942° | 2025-09-19 05:31:12.599Z | 44.103° NE |
4 mins | 2025-09-19 07:06:12.599Z | 315.497° NNW | 2025-09-19 07:08:12.599Z | 351.836° N | 16.797° | 2025-09-19 07:10:12.599Z | 22.717° NE |
5 mins | 2025-09-19 10:27:12.599Z | 342.912° N | 2025-09-19 10:29:12.599Z | 23.786° NE | 23.205° | 2025-09-19 10:32:12.599Z | 78.198° E |
6 mins | 2025-09-19 12:06:12.599Z | 300.722° NW | 2025-09-19 12:09:12.599Z | 210.268° SW | 41.586° | 2025-09-19 12:12:12.599Z | 144.922° SSE |
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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