HAWK-8A, 59443
Orbit data source: Space-Track
HAWK-8A, 59443 is a payload satellite owned by HawkEye 360 (US) in LEO that was launched on Sun, 07 Apr 2024 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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59443 intel report (Beta)
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Expand to show TLE details & historyLast TLE update: 19 hours ago
TLE from 19 hours ago
0 HAWK-8A
1 59443U 24066B 25293.79628685 .00005078 00000-0 44363-3 0 9998
2 59443 45.5933 73.3371 0004772 227.6436 132.4041 14.97916153 83923
TLE epoch observation values (Epoch: 2025-10-20T19:06:39.183Z)
Visualization orbit readout
Visualization observer readout
Orbital elements
Other satellites on launch #66 in the year 2024 (2024-04-07 UTC)
HAWK-8A 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 | 2025-10-21 14:36:46.388Z | 279.826° WNW | 2025-10-21 14:39:46.388Z | 329.526° NNW | 33.462° | 2025-10-21 14:43:46.388Z | 59.403° ENE |
6 mins | 2025-10-21 16:18:46.388Z | 304.906° NW | 2025-10-21 16:21:46.388Z | 15.858° NNE | 33.519° | 2025-10-21 16:24:46.388Z | 75.642° E |
7 mins | 2025-10-21 17:59:46.388Z | 292.37° WNW | 2025-10-21 18:02:46.388Z | 174.397° S | 44.453° | 2025-10-21 18:06:46.388Z | 120.773° SE |
5 mins | 2025-10-22 11:18:46.388Z | 175.196° S | 2025-10-22 11:20:46.388Z | 136.242° SSE | 21.485° | 2025-10-22 11:23:46.388Z | 89.187° E |
7 mins | 2025-10-22 12:57:46.388Z | 248.647° W | 2025-10-22 13:00:46.388Z | 279.864° WNW | 44.091° | 2025-10-22 13:04:46.388Z | 63.693° ENE |
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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