EAGLEEYE, 60508 (Decayed)
Orbit data source: Space-Track
EAGLEEYE, 60508 was a Polish payload satellite in LEO 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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60508 intel report (Beta)
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Identifier
Orbit
Country
PL / POLRelated business
Manufacturer
CREO
Mission
Decayed Commercial Imaging
Bus & Motor
HYPERSAT, Unknown motor
Mass
55 kg wet, 55 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Box + 2 Pan, 0.8 m
Radar Cross Section
0.714 m², Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 1 month ago
TLE from 1 month ago
0 EAGLEEYE
1 60508U 24149AS 26266.32291028 .12422171 25427-5 23333-3 0 9990
2 60508 97.3364 7.3674 0013278 273.1936 86.7847 16.46500711118496Epoch: 2026-09-23T07:44Z
TLE epoch observation values (Epoch: 2026-09-23T07:44:59.448Z)
Latitude
-0.00008°
Longitude
-111.05598°
Altitude
151.354 km
Speed
7.816 km/s
True Right ascension
00h 29m 28s
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
01:14:49
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
154.025 km
Perigee altitude
136.701 km
Semi-major axis
6,523.5 km
Eccentricity
0.00133
Inclination
97.3364°
RAAN
7.3674°
Arg. of periapsis
273.1936°
True anomaly
86.93663°
Mean anomaly
86.7847°
Eccentric anomaly
86.86066°
Mean motion
4.11929 °/min
Orbital period
87.39 mins
BSTAR
0.00023333
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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.EAGLEEYE Visibility
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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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| This satellite is decayed. |
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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