STARLINK-5685, 55477
Orbit data source: Space-Track
STARLINK-5685, 55477 is a payload satellite owned by SpaceX/Seattle (US) in LEO that was launched on Thu, 02 Feb 2023 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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55477 intel report (Beta)
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Expand to show TLE details & historyLast TLE update: 18 hours ago
TLE from 18 hours ago
0 STARLINK-5685
1 55477U 23015AE 25255.56721388 .00000290 00000-0 36535-4 0 9995
2 55477 43.0024 201.3713 0001145 272.6259 87.4452 15.02538241144105
TLE epoch observation values (Epoch: 2025-09-12T13:36:47.279Z)
Visualization orbit readout
Visualization observer readout
Orbital elements
Other satellites on launch #15 in the year 2023 (2023-02-02 UTC)
STARLINK-5685 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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7 mins | 2025-09-13 23:18:39.502Z | 215.444° SW | 2025-09-13 23:22:39.502Z | 134.104° SE | 30.584° | 2025-09-13 23:25:39.502Z | 84.306° E |
7 mins | 2025-09-14 00:59:39.502Z | 262.871° W | 2025-09-14 01:02:39.502Z | 331.992° NNW | 43.594° | 2025-09-14 01:06:39.502Z | 71.055° E |
7 mins | 2025-09-14 02:40:39.502Z | 289.054° WNW | 2025-09-14 02:43:39.502Z | 1.331° NNE | 39.88° | 2025-09-14 02:47:39.502Z | 83.457° E |
7 mins | 2025-09-14 04:21:39.502Z | 284.23° WNW | 2025-09-14 04:24:39.502Z | 180.619° SSW | 43.617° | 2025-09-14 04:28:39.502Z | 117.95° SE |
4 mins | 2025-09-14 06:03:39.502Z | 237.443° WSW | 2025-09-14 06:04:39.502Z | 219.023° SW | 17.772° | 2025-09-14 06:07:39.502Z | 172.954° S |
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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