HAWK-9B, 59450
Orbit data source: Space-Track
HAWK-9B, 59450 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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59450 intel report (Beta)
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Expand to show TLE details & historyLast TLE update: 1 day ago
TLE from 1 day ago
0 HAWK-9B
1 59450U 24066J 25261.33256638 .00002355 00000-0 21819-3 0 9992
2 59450 45.6206 241.6318 0004178 0.2280 359.8603 14.97523614 79052
TLE epoch observation values (Epoch: 2025-09-18T07:58:53.735Z)
Visualization orbit readout
Visualization observer readout
Orbital elements
Other satellites on launch #66 in the year 2024 (2024-04-07 UTC)
HAWK-9B 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 | 2025-09-19 08:31:28.296Z | 271.004° WNW | 2025-09-19 08:34:28.296Z | 215.779° SW | 24.987° | 2025-09-19 08:37:28.296Z | 163.935° S |
7 mins | 2025-09-20 01:49:28.296Z | 231.789° WSW | 2025-09-20 01:52:28.296Z | 164.466° S | 43.071° | 2025-09-20 01:56:28.296Z | 68.559° E |
6 mins | 2025-09-20 03:31:28.296Z | 290.71° WNW | 2025-09-20 03:33:28.296Z | 344.517° N | 34.597° | 2025-09-20 03:37:28.296Z | 61.17° ENE |
6 mins | 2025-09-20 05:12:28.296Z | 308.283° NW | 2025-09-20 05:14:28.296Z | 350.647° N | 32.429° | 2025-09-20 05:18:28.296Z | 76.956° E |
6 mins | 2025-09-20 06:53:28.296Z | 293.159° NW | 2025-09-20 06:56:28.296Z | 133.236° SE | 43.189° | 2025-09-20 06:59:28.296Z | 119.435° SE |
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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