STARLINK-1656, 46353
Orbit data source: Space-Track
STARLINK-1656, 46353 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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46353 intel report (Beta)
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Expand to show TLE details & historyLast TLE update: 19 hours ago
TLE from 19 hours ago
0 STARLINK-1656
1 46353U 20062AE 25256.26475842 .00000177 00000-0 30763-4 0 9997
2 46353 53.0552 93.1124 0001353 89.9374 270.1770 15.06394779277567
TLE epoch observation values (Epoch: 2025-09-13T06:21:15.127Z)
Visualization orbit readout
Visualization observer readout
Orbital elements
Other satellites on launch #62 in the year 2020 (2020-09-03 UTC)
STARLINK-1656 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 | 2025-09-14 14:20:42.401Z | 164.424° S | 2025-09-14 14:22:42.401Z | 135.07° SSE | 15.219° | 2025-09-14 14:24:42.401Z | 101.034° ESE |
6 mins | 2025-09-14 15:59:42.401Z | 241.894° WSW | 2025-09-14 16:02:42.401Z | 4.021° NNE | 41.701° | 2025-09-14 16:05:42.401Z | 45° ENE |
4 mins | 2025-09-14 17:40:42.401Z | 310.702° NW | 2025-09-14 17:42:42.401Z | 347.119° N | 17.607° | 2025-09-14 17:44:42.401Z | 19.986° NNE |
5 mins | 2025-09-14 21:01:42.401Z | 340.339° N | 2025-09-14 21:03:42.401Z | 17.741° NNE | 22.027° | 2025-09-14 21:06:42.401Z | 73.67° E |
6 mins | 2025-09-14 22:41:42.401Z | 300.381° NW | 2025-09-14 22:43:42.401Z | 237.601° WSW | 43.129° | 2025-09-14 22:47:42.401Z | 139.581° 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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