HAWK-9A, 59446
Orbit data source: Space-Track
HAWK-9A, 59446 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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59446 intel report (Beta)
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Edit Public Description
Identifier
Orbit
Country
USRelated business
Manufacturer
UTIAS-SFL
Mission
Operational Commercial Sigint
Bus & Motor
HAWK2G, Unknown motor
Mass
31 kg wet, 30 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Box + 2 Pan, 1.0 m
Radar Cross Section
0.240 m², Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 19 hours ago
TLE from 19 hours ago
0 HAWK-9A
1 59446U 24066E 25293.81687762 .00004985 00000-0 43663-3 0 9993
2 59446 45.6085 73.4722 0004229 218.9735 141.0841 14.97849989 83924Epoch: 2025-10-20T19:36Z
TLE epoch observation values (Epoch: 2025-10-20T19:36:18.226Z)
Latitude
-0.00004°
Longitude
109.88247°
Altitude
575.894 km
Speed
7.573 km/s
True Right ascension
04h 53m 53s
True Declination
0° 00' 00"
Sunlit
Visualization orbit readout
Latitude
Unknown
Longitude
Unknown
Altitude
Unknown
Speed
Unknown
Apparent Right ascension
Unknown
Apparent Declination
Unknown
Sunlit
Visualization observer readout
Local Sidereal Time
09:09:52
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
577.969 km
Perigee altitude
572.088 km
Semi-major axis
6,953.165 km
Eccentricity
0.00042
Inclination
45.6085°
RAAN
73.4722°
Arg. of periapsis
218.9735°
True anomaly
141.11453°
Mean anomaly
141.0841°
Eccentric anomaly
141.09932°
Mean motion
3.74343 °/min
Orbital period
96.17 mins
BSTAR
0.00043663
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Other satellites on launch #66 in the year 2024 (2024-04-07 UTC)
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You can import UDL-sourced sensor .json files into the Sandbox to generate a visibility chart that accounts for multi-vendor sensor geometry.HAWK-9A 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. |
|---|---|---|---|---|---|---|---|
| 7 mins | 2025-10-21 15:08:14.237Z | 289.753° WNW | 2025-10-21 15:11:14.237Z | 344.183° N | 31.7° | 2025-10-21 15:15:14.237Z | 63.397° ENE |
| 6 mins | 2025-10-21 16:50:14.237Z | 306.8° NW | 2025-10-21 16:53:14.237Z | 33.507° NE | 36.53° | 2025-10-21 16:56:14.237Z | 87.379° E |
| 6 mins | 2025-10-21 18:31:14.237Z | 280.028° WNW | 2025-10-21 18:33:14.237Z | 237.229° WSW | 37.255° | 2025-10-21 18:37:14.237Z | 138.028° SSE |
| 6 mins | 2025-10-22 11:49:14.237Z | 199.728° SSW | 2025-10-22 11:51:14.237Z | 157.065° SSE | 30.709° | 2025-10-22 11:55:14.237Z | 78.752° E |
| 7 mins | 2025-10-22 13:29:14.237Z | 264.751° W | 2025-10-22 13:32:14.237Z | 337.544° N | 40.757° | 2025-10-22 13:36:14.237Z | 61.166° 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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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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