STARLINK-1402, 45685
Orbit data source: Space-Track
STARLINK-1402, 45685 is a payload satellite owned by SpaceX/Seattle (US) in LEO that was launched on Thu, 04 Jun 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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45685 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-1402
1 45685U 20035AE 25260.84027735 .00001614 00000-0 12715-3 0 9990
2 45685 53.0545 106.9886 0001272 120.9138 239.1977 15.06411898292909
TLE epoch observation values (Epoch: 2025-09-17T20:09:59.963Z)
Visualization orbit readout
Visualization observer readout
Orbital elements
Other satellites on launch #35 in the year 2020 (2020-06-04 UTC)
STARLINK-1402 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 | 2025-09-18 15:25:16.033Z | 176.742° S | 2025-09-18 15:28:16.033Z | 125.121° SE | 20.549° | 2025-09-18 15:31:16.033Z | 77.646° E |
6 mins | 2025-09-18 17:05:16.033Z | 258.908° W | 2025-09-18 17:07:16.033Z | 319.297° NNW | 38.2° | 2025-09-18 17:11:16.033Z | 42.132° NE |
4 mins | 2025-09-18 18:46:16.033Z | 320.959° NNW | 2025-09-18 18:47:16.033Z | 337.92° N | 15.78° | 2025-09-18 18:50:16.033Z | 25.067° NE |
5 mins | 2025-09-18 22:07:16.033Z | 344.481° N | 2025-09-18 22:09:16.033Z | 30.839° NE | 25.622° | 2025-09-18 22:12:16.033Z | 85.079° E |
6 mins | 2025-09-18 23:46:16.033Z | 293.381° NW | 2025-09-18 23:49:16.033Z | 201.415° SSW | 36.45° | 2025-09-18 23:52:16.033Z | 151.656° 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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