STARLINK-5688, 55479
Orbit data source: Space-Track
STARLINK-5688, 55479 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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55479 intel report (Beta)
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Expand to show TLE details & historyLast TLE update: 15 hours ago
TLE from 15 hours ago
0 STARLINK-5688
1 55479U 23015AG 25288.28320014 .00000494 00000-0 51677-4 0 9993
2 55479 43.0042 23.7168 0001553 268.3915 91.6749 15.02534075149024
TLE epoch observation values (Epoch: 2025-10-15T06:47:48.492Z)
Visualization orbit readout
Visualization observer readout
Orbital elements
Other satellites on launch #15 in the year 2023 (2023-02-02 UTC)
STARLINK-5688 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 | 2025-10-16 08:30:31.307Z | 167.003° S | 2025-10-16 08:32:31.307Z | 134.124° SE | 15.26° | 2025-10-16 08:34:31.307Z | 104.865° ESE |
6 mins | 2025-10-16 10:09:31.307Z | 233.929° WSW | 2025-10-16 10:12:31.307Z | 133.645° SE | 41.878° | 2025-10-16 10:15:31.307Z | 76.705° E |
6 mins | 2025-10-16 11:50:31.307Z | 280.478° WNW | 2025-10-16 11:53:31.307Z | 25.215° NE | 38.967° | 2025-10-16 11:56:31.307Z | 71.802° E |
6 mins | 2025-10-16 13:31:31.307Z | 293.378° NW | 2025-10-16 13:33:31.307Z | 329.272° NNW | 41.199° | 2025-10-16 13:37:31.307Z | 94.461° ESE |
6 mins | 2025-10-16 15:12:31.307Z | 266.31° W | 2025-10-16 15:14:31.307Z | 212.157° SW | 34.229° | 2025-10-16 15:18:31.307Z | 137.823° 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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