HAWK-9C, 59448
Orbit data source: Space-Track
HAWK-9C, 59448 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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59448 intel report (Beta)
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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: 16 hours ago
TLE from 16 hours ago
0 HAWK-9C
1 59448U 24066G 26306.92673569 .00000931 00000-0 93355-4 0 9994
2 59448 45.6099 279.0243 0002572 21.8499 338.2492 14.99492496140655Epoch: 2026-11-02T22:14Z
TLE epoch observation values (Epoch: 2026-11-02T22:14:29.963Z)
Latitude
-0.00001°
Longitude
-96.79729°
Altitude
566.87 km
Speed
7.58 km/s
True Right ascension
18h 36m 05s
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
10:26:02
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
571.739 km
Perigee altitude
568.165 km
Semi-major axis
6,948.089 km
Eccentricity
0.00026
Inclination
45.6099°
RAAN
279.0243°
Arg. of periapsis
21.8499°
True anomaly
338.23827°
Mean anomaly
338.2492°
Eccentric anomaly
338.24374°
Mean motion
3.74753 °/min
Orbital period
96.06 mins
BSTAR
0.000093355
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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-9C 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. |
|---|---|---|---|---|---|---|---|
| 4 mins | 2026-11-03 23:59:02.560Z | 171.626° S | 2026-11-04 00:01:02.560Z | 143.343° SSE | 14.997° | 2026-11-04 00:03:02.560Z | 111.666° ESE |
| 6 mins | 2026-11-04 01:39:02.560Z | 232.865° WSW | 2026-11-04 01:42:02.560Z | 102.219° ESE | 66.044° | 2026-11-04 01:45:02.560Z | 68.261° E |
| 6 mins | 2026-11-04 03:20:02.560Z | 288.492° WNW | 2026-11-04 03:22:02.560Z | 331.933° NNW | 40.965° | 2026-11-04 03:26:02.560Z | 59.355° ENE |
| 6 mins | 2026-11-04 05:01:02.560Z | 306.782° NW | 2026-11-04 05:04:02.560Z | 22.024° NNE | 40.187° | 2026-11-04 05:07:02.560Z | 76.376° E |
| 6 mins | 2026-11-04 06:42:02.560Z | 292.569° NW | 2026-11-04 06:45:02.560Z | 142.161° SSE | 70.916° | 2026-11-04 06:48:02.560Z | 120.853° SE |
| 4 mins | 2026-11-04 08:23:02.560Z | 252.056° W | 2026-11-04 08:25:02.560Z | 218.816° SW | 17.351° | 2026-11-04 08:27:02.560Z | 187.668° SSW |
Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
Click to sort rows by RSO header in ascending order | Click to sort rows by Country header in ascending order | Click to sort rows by Type header in ascending order | Click to sort rows by Inclination Δ header in ascending order | Click to sort rows by RAAN Δ header in ascending order | Click to sort rows by Coplanar Angle header in ascending order | Click to sort rows by SMA Δ header in ascending order | Click to sort rows by Orbital period header in ascending order | Click to sort rows by <5km Md TCA header in descending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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