HAWK-10A, 60540
Orbit data source: Space-Track
HAWK-10A, 60540 is a payload satellite owned by HawkEye 360 (US) in SSO that was launched on Fri, 16 Aug 2024 UTC via an FALCON 9 launch vehicle from the Air Force Western Test Range (AFWTR). 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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60540 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: 19 hours ago
TLE from 19 hours ago
0 HAWK-10A
1 60540U 24149CA 26175.19023161 .00000742 00000-0 70287-4 0 9990
2 60540 97.6894 250.9815 0004514 60.3953 299.7718 14.96531916101033Epoch: 2026-06-24T04:33Z
TLE epoch observation values (Epoch: 2026-06-24T04:33:56.011Z)
Latitude
0.00002°
Longitude
-89.85288°
Altitude
579.114 km
Speed
7.572 km/s
True Right ascension
16h 43m 55s
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
10:49:01
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
577.77 km
Perigee altitude
571.493 km
Semi-major axis
6,952.768 km
Eccentricity
0.00045
Inclination
97.6894°
RAAN
250.9815°
Arg. of periapsis
60.3953°
True anomaly
299.72689°
Mean anomaly
299.7718°
Eccentric anomaly
299.74935°
Mean motion
3.74375 °/min
Orbital period
96.16 mins
BSTAR
0.000070287
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Other satellites on launch #149 in the year 2024 (2024-08-16 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-10A 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 | 2026-06-25 04:45:57.958Z | 146.563° SSE | 2026-06-25 04:48:57.958Z | 85.786° E | 37.59° | 2026-06-25 04:52:57.958Z | 358.888° N |
| 6 mins | 2026-06-25 18:02:57.958Z | 8.169° NNE | 2026-06-25 18:05:57.958Z | 231.671° WSW | 43.681° | 2026-06-25 18:08:57.958Z | 198.236° 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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