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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TLE from 14 hours ago
0 STARLINK-1656
1 46353U 20062AE 25199.40544811 .00000225 00000-0 33969-4 0 9997
2 46353 53.0572 348.3634 0001237 91.6260 268.4870 15.06400889268993
TLE epoch observation values (Epoch: 2025-07-18T09:43:50.716Z)
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
Observer location: undefined°, undefined°
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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5 mins | 2025-07-19 11:21:04.131Z | 173.474° S | 2025-07-19 11:24:04.131Z | 124.863° SE | 18.491° | 2025-07-19 11:26:04.131Z | 90.34° ESE |
6 mins | 2025-07-19 13:01:04.131Z | 254.012° W | 2025-07-19 13:03:04.131Z | 320.293° NNW | 40.256° | 2025-07-19 13:07:04.131Z | 43.68° NE |
4 mins | 2025-07-19 14:42:04.131Z | 320.738° NNW | 2025-07-19 14:43:04.131Z | 338.359° N | 16.472° | 2025-07-19 14:46:04.131Z | 25.684° NE |
5 mins | 2025-07-19 18:03:04.131Z | 346.351° N | 2025-07-19 18:05:04.131Z | 31.351° NE | 24.141° | 2025-07-19 18:08:04.131Z | 82.764° E |
6 mins | 2025-07-19 19:42:04.131Z | 296.678° NW | 2025-07-19 19:45:04.131Z | 194.401° SSW | 38.718° | 2025-07-19 19:48:04.131Z | 147.315° 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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Event ID | Pc | Md | Secondary | Secondary name | Country | Click to unsort rows by TCA header |
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