STARLINK-5690, 55480
Orbit data source: Space-Track
STARLINK-5690, 55480 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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55480 intel report (Beta)
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Expand to show TLE details & historyLast TLE update: 1 day ago
TLE from 1 day ago
0 STARLINK-5690
1 55480U 23015AH 25255.19767119 -.00000014 00000-0 14017-4 0 9996
2 55480 43.0038 228.8166 0001200 266.6415 93.4291 15.02537772143755
TLE epoch observation values (Epoch: 2025-09-12T04:44:38.79Z)
Visualization orbit readout
Visualization observer readout
Orbital elements
Other satellites on launch #15 in the year 2023 (2023-02-02 UTC)
STARLINK-5690 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 | 2025-09-13 08:25:34.724Z | 248.438° W | 2025-09-13 08:27:34.724Z | 218.593° SW | 13.7° | 2025-09-13 08:29:34.724Z | 189.407° SSW |
6 mins | 2025-09-14 01:39:34.724Z | 230.989° WSW | 2025-09-14 01:41:34.724Z | 190.247° SSW | 40.573° | 2025-09-14 01:45:34.724Z | 76.202° E |
6 mins | 2025-09-14 03:20:34.724Z | 282.296° WNW | 2025-09-14 03:22:34.724Z | 339.879° N | 40.31° | 2025-09-14 03:26:34.724Z | 72.747° E |
7 mins | 2025-09-14 05:00:34.724Z | 290.805° WNW | 2025-09-14 05:03:34.724Z | 356.832° N | 42.492° | 2025-09-14 05:07:34.724Z | 94.488° ESE |
6 mins | 2025-09-14 06:41:34.724Z | 273.741° WNW | 2025-09-14 06:44:34.724Z | 197.543° SSW | 34.633° | 2025-09-14 06:47:34.724Z | 140.128° 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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