STARLINK-1719, 46331
Orbit data source: Space-Track
STARLINK-1719, 46331 is a payload satellite owned by SpaceX/Seattle (US) in LEO that was launched on Thu, 03 Sep 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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46331 intel report (Beta)
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Expand to show TLE details & historyLast TLE update: 12 hours ago
TLE from 12 hours ago
0 STARLINK-1719
1 46331U 20062G 25288.00002315 .02044972 00000-0 72848-1 0 9991
2 46331 53.0555 309.9785 0001136 74.5945 205.4852 15.24966834 5850
TLE epoch observation values (Epoch: 2025-10-15T00:00:02.000Z)
Visualization orbit readout
Visualization observer readout
Orbital elements
Other satellites on launch #62 in the year 2020 (2020-09-03 UTC)
STARLINK-1719 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 | 2025-10-15 11:52:55.432Z | 291.658° WNW | 2025-10-15 11:55:55.432Z | 217.789° SW | 32.145° | 2025-10-15 11:58:55.432Z | 158.297° S |
4 mins | 2025-10-16 03:12:55.432Z | 172.35° S | 2025-10-16 03:14:55.432Z | 128.603° SE | 21.741° | 2025-10-16 03:16:55.432Z | 86.321° E |
5 mins | 2025-10-16 04:50:55.432Z | 270.252° WNW | 2025-10-16 04:52:55.432Z | 339.597° N | 33.096° | 2025-10-16 04:55:55.432Z | 37.512° NE |
4 mins | 2025-10-16 09:47:55.432Z | 347.517° N | 2025-10-16 09:49:55.432Z | 38.855° NE | 23.617° | 2025-10-16 09:51:55.432Z | 79.484° E |
5 mins | 2025-10-16 11:25:55.432Z | 282.364° WNW | 2025-10-16 11:27:55.432Z | 206.367° SW | 34.116° | 2025-10-16 11:30:55.432Z | 153.016° 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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