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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: 7 hours ago

TLE from 7 hours ago
0 EAGLEEYE
1 60508U 24149AS  26051.85382211  .00049387  00000-0  75084-3 0  9991
2 60508  97.3802 140.2899 0002564 323.7739  36.3341 15.54402451 84771
Epoch: 2026-02-20T20:29Z
TLE epoch observation values (Epoch: 2026-02-20T20:29:30.230Z)
Latitude
0.00001°
Longitude
42.12915°
Altitude
405.627 km
Speed
7.668 km/s
True Right ascension
09h 21m 09s
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
06:23:19
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
402.547 km
Perigee altitude
399.071 km
Semi-major axis
6,778.946 km
Eccentricity
0.00026
Inclination
97.3802°
RAAN
140.2899°
Arg. of periapsis
323.7739°
True anomaly
36.35151°
Mean anomaly
36.3341°
Eccentric anomaly
36.34281°
Mean motion
3.88866 °/min
Orbital period
92.58 mins
BSTAR
0.00075084
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