EAGLEEYE, 60508
Orbit data source: Space-Track
EAGLEEYE, 60508 is a Polish payload satellite 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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60508 intel report (Beta)
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Edit Public Description
Identifier
Orbit
Country
PL / POLRelated business
Manufacturer
CREO
Mission
Operational 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 day ago
TLE from 1 day ago
0 EAGLEEYE
1 60508U 24149AS 25287.19812089 .00038429 00000-0 92600-3 0 9997
2 60508 97.3979 7.8664 0004407 83.0439 277.1309 15.41141566 64720Epoch: 2025-10-14T04:45Z
TLE epoch observation values (Epoch: 2025-10-14T04:45:17.644Z)
Latitude
-0.00003°
Longitude
-86.44711°
Altitude
445.486 km
Speed
7.645 km/s
True Right ascension
00h 31m 27s
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
09:07:39
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
442.681 km
Perigee altitude
436.672 km
Semi-major axis
6,817.813 km
Eccentricity
0.00044
Inclination
97.3979°
RAAN
7.8664°
Arg. of periapsis
83.0439°
True anomaly
277.08079°
Mean anomaly
277.1309°
Eccentric anomaly
277.10584°
Mean motion
3.85545 °/min
Orbital period
93.37 mins
BSTAR
0.000926
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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 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. |
|---|---|---|---|---|---|---|---|
| 5 mins | 2025-10-15 18:42:37.380Z | 354.317° N | 2025-10-15 18:45:37.380Z | 259.053° W | 32.769° | 2025-10-15 18:47:37.380Z | 217.153° SW |
| 4 mins | 2025-10-16 05:12:37.380Z | 132.544° SE | 2025-10-16 05:14:37.380Z | 55.429° ENE | 32.934° | 2025-10-16 05:16:37.380Z | 7.791° NNE |
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 ascending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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