STARLINK-5764, 55602
Orbit data source: Space-Track
STARLINK-5764, 55602 is a payload satellite owned by SpaceX/Seattle (US) in LEO that was launched on Sun, 12 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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55602 intel report (Beta)
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Expand to show TLE details & historyLast TLE update: 2 days ago
TLE from 2 days ago
0 STARLINK-5764
1 55602U 23020AK 25259.31240733 .00000840 00000-0 77260-4 0 9999
2 55602 43.0034 219.5755 0001018 273.7522 86.3204 15.02538043142838
TLE epoch observation values (Epoch: 2025-09-16T07:29:51.993Z)
Visualization orbit readout
Visualization observer readout
Orbital elements
Other satellites on launch #20 in the year 2023 (2023-02-12 UTC)
STARLINK-5764 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 | 2025-09-17 23:33:48.624Z | 191.461° SSW | 2025-09-17 23:36:48.624Z | 140.251° SSE | 20.764° | 2025-09-17 23:39:48.624Z | 93.411° ESE |
7 mins | 2025-09-18 01:13:48.624Z | 246.539° WSW | 2025-09-18 01:16:48.624Z | 199.754° SSW | 44.655° | 2025-09-18 01:20:48.624Z | 72.698° E |
7 mins | 2025-09-18 02:54:48.624Z | 283.357° WNW | 2025-09-18 02:57:48.624Z | 359.13° N | 39.498° | 2025-09-18 03:01:48.624Z | 76.493° E |
7 mins | 2025-09-18 04:35:48.624Z | 290.16° WNW | 2025-09-18 04:38:48.624Z | 38.547° NE | 44.431° | 2025-09-18 04:42:48.624Z | 103.389° ESE |
6 mins | 2025-09-18 06:16:48.624Z | 263.439° W | 2025-09-18 06:18:48.624Z | 223.117° SW | 27.299° | 2025-09-18 06:22:48.624Z | 150.001° 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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