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: 21 hours ago
TLE from 21 hours ago
0 EAGLEEYE
1 60508U 24149AS 25309.19562660 .00038943 00000-0 88157-3 0 9992
2 60508 97.3978 30.1719 0003297 6.1317 353.9970 15.43022088 68119Epoch: 2025-11-05T04:41Z
TLE epoch observation values (Epoch: 2025-11-05T04:41:42.138Z)
Latitude
-0.00004°
Longitude
-84.92545°
Altitude
438.083 km
Speed
7.65 km/s
True Right ascension
02h 00m 41s
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
21:27:42
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
436.377 km
Perigee altitude
431.885 km
Semi-major axis
6,812.268 km
Eccentricity
0.00033
Inclination
97.3978°
RAAN
30.1719°
Arg. of periapsis
6.1317°
True anomaly
353.99305°
Mean anomaly
353.997°
Eccentric anomaly
353.99502°
Mean motion
3.86016 °/min
Orbital period
93.26 mins
BSTAR
0.00088157
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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. |
|---|---|---|---|---|---|---|---|
| 6 mins | 2025-11-06 05:43:05.259Z | 175.99° S | 2025-11-06 05:46:05.259Z | 251.048° W | 42.442° | 2025-11-06 05:49:05.259Z | 341.556° N |
| 5 mins | 2025-11-06 18:37:05.259Z | 357.126° N | 2025-11-06 18:39:05.259Z | 265.096° W | 40.347° | 2025-11-06 18:42:05.259Z | 204.345° SW |
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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