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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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Identifier
60508, 2024-149AS
Orbit
SSO
Country
Flag of PLPL / POL
Related business
Manufacturer
CREO
Mission
Operational Commercial Imaging
Bus & Motor
HYPERSAT, Unknown motor
Mass
55 kg wet, 55 kg dry
Launch date (UTC)
2024-08-16 (2 years ago)
Launch vehicle
FALCON 9
Launch site
Air Force Western Test Range (AFWTR)
Object type
Payload
Rocket body
Debris
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 & history
Last TLE update: 14 hours ago

TLE from 14 hours ago
0 EAGLEEYE
1 60508U 24149AS  26124.49606509  .00071482  00000-0  74892-3 0  9998
2 60508  97.3727 215.6722 0002544  84.3622 275.7927 15.64181792 96098
Epoch: 2026-05-04T11:54Z
TLE epoch observation values (Epoch: 2026-05-04T11:54:20.023Z)
Latitude
-0.00005°
Longitude
174.70435°
Altitude
378.571 km
Speed
7.683 km/s
True Right ascension
14h 22m 41s
True Declination
0° 00' 00"
Sunlit
Object was in full shadow at epoch
Visualization orbit readout
Latitude
Unknown
Longitude
Unknown
Altitude
Unknown
Speed
Unknown
Apparent Right ascension
Unknown
Apparent Declination
Unknown
Sunlit
N/A
Visualization observer readout
Local Sidereal Time
10:13:27
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
374.216 km
Perigee altitude
370.781 km
Semi-major axis
6,750.636 km
Eccentricity
0.00025
Inclination
97.3727°
RAAN
215.6722°
Arg. of periapsis
84.3622°
True anomaly
275.7637°
Mean anomaly
275.7927°
Eccentric anomaly
275.7782°
Mean motion
3.91315 °/min
Orbital period
92 mins
BSTAR
0.00074892
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