HAWK-8C, 59449
Orbit data source: Space-Track
HAWK-8C, 59449 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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59449 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-8C
1 59449U 24066H 25293.79619762 .00004985 00000-0 43588-3 0 9994
2 59449 45.6063 74.0137 0004393 232.4016 127.6466 14.97914726 83919
TLE epoch observation values (Epoch: 2025-10-20T19:06:31.474Z)
Visualization orbit readout
Visualization observer readout
Orbital elements
Other satellites on launch #66 in the year 2024 (2024-04-07 UTC)
HAWK-8C 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 14:36:46.057Z | 280.602° WNW | 2025-10-21 14:39:46.057Z | 339.695° N | 34.518° | 2025-10-21 14:43:46.057Z | 60.667° ENE |
6 mins | 2025-10-21 16:18:46.057Z | 307.311° NW | 2025-10-21 16:21:46.057Z | 25.608° NE | 32.576° | 2025-10-21 16:24:46.057Z | 76.524° E |
6 mins | 2025-10-21 17:59:46.057Z | 293.058° NW | 2025-10-21 18:02:46.057Z | 136.926° SSE | 43.58° | 2025-10-21 18:05:46.057Z | 119.655° SE |
4 mins | 2025-10-22 11:18:46.057Z | 170.23° S | 2025-10-22 11:20:46.057Z | 130.98° SE | 20.451° | 2025-10-22 11:22:46.057Z | 97.675° ESE |
7 mins | 2025-10-22 12:57:46.057Z | 247.349° WSW | 2025-10-22 13:00:46.057Z | 325.798° NNW | 44.859° | 2025-10-22 13:04:46.057Z | 64.259° 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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