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 25260.11704276 .00001666 00000-0 13836-3 0 9999
2 55480 43.0028 202.0849 0001121 267.9283 92.1431 15.02539367144491
TLE epoch observation values (Epoch: 2025-09-17T02:48:32.494Z)
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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5 mins | 2025-09-18 22:03:40.283Z | 181.965° SSW | 2025-09-18 22:06:40.283Z | 133.101° SE | 17.065° | 2025-09-18 22:08:40.283Z | 102.753° ESE |
6 mins | 2025-09-18 23:43:40.283Z | 238.541° WSW | 2025-09-18 23:46:40.283Z | 124.286° SE | 43.004° | 2025-09-18 23:49:40.283Z | 75.152° E |
6 mins | 2025-09-19 01:24:40.283Z | 282.789° WNW | 2025-09-19 01:27:40.283Z | 25.186° NE | 38.602° | 2025-09-19 01:30:40.283Z | 72.661° E |
6 mins | 2025-09-19 03:05:40.283Z | 292.751° NW | 2025-09-19 03:07:40.283Z | 325.267° NNW | 41.864° | 2025-09-19 03:11:40.283Z | 97.445° ESE |
5 mins | 2025-09-19 04:46:40.283Z | 262.915° W | 2025-09-19 04:48:40.283Z | 210.927° SW | 31.779° | 2025-09-19 04:51:40.283Z | 147.617° 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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