HAWK-8B, 59445
Orbit data source: Space-Track
HAWK-8B, 59445 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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59445 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-8B
1 59445U 24066D 25293.79665558 .00005103 00000-0 44574-3 0 9993
2 59445 45.6188 74.6899 0004704 230.2601 129.7865 14.97918378 83919
TLE epoch observation values (Epoch: 2025-10-20T19:07:11.042Z)
Visualization orbit readout
Visualization observer readout
Orbital elements
Other satellites on launch #66 in the year 2024 (2024-04-07 UTC)
HAWK-8B 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 14:37:15.519Z | 279.555° WNW | 2025-10-21 14:40:15.519Z | 336.696° NNW | 34.602° | 2025-10-21 14:44:15.519Z | 60.209° ENE |
6 mins | 2025-10-21 16:19:15.519Z | 306.669° NW | 2025-10-21 16:22:15.519Z | 22.915° NE | 32.548° | 2025-10-21 16:25:15.519Z | 75.488° E |
6 mins | 2025-10-21 18:00:15.519Z | 293.884° NW | 2025-10-21 18:03:15.519Z | 132.363° SE | 44.062° | 2025-10-21 18:06:15.519Z | 118.463° SE |
4 mins | 2025-10-22 11:19:15.519Z | 170.546° S | 2025-10-22 11:21:15.519Z | 132.537° SE | 19.977° | 2025-10-22 11:23:15.519Z | 99.051° ESE |
7 mins | 2025-10-22 12:58:15.519Z | 246.128° WSW | 2025-10-22 13:01:15.519Z | 290.117° WNW | 44.879° | 2025-10-22 13:05:15.519Z | 64.462° 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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