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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: 20 hours ago

TLE from 20 hours ago
0 EAGLEEYE
1 60508U 24149AS  26083.80445388  .00058588  00000-0  75816-3 0  9992
2 60508  97.3749 173.3178 0003779 200.2285 159.8822 15.58723813 89741
Epoch: 2026-03-24T19:18Z
TLE epoch observation values (Epoch: 2026-03-24T19:18:24.815Z)
Latitude
-0.00001°
Longitude
61.43755°
Altitude
396.896 km
Speed
7.671 km/s
True Right ascension
11h 33m 16s
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
20:31:00
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
390.82 km
Perigee altitude
385.706 km
Semi-major axis
6,766.4 km
Eccentricity
0.00038
Inclination
97.3749°
RAAN
173.3178°
Arg. of periapsis
200.2285°
True anomaly
159.89709°
Mean anomaly
159.8822°
Eccentric anomaly
159.88964°
Mean motion
3.89948 °/min
Orbital period
92.32 mins
BSTAR
0.00075816
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