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NORAD ID: 60508 • Int'l Des: 2024-149 • Owner: CREO • Country: PL • operational
LEOCIRCULARRETROGRADESSO
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About EagleEye
EagleEye (NORAD 60508) is a satellite launched Aug 16, 2024 by CREO of PL. It operates in LEO, CIRCULAR, RETROGRADE, SSO orbit with a mass of 55.00 kg.
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Two-Line Element Set
1 60508U 24149AS 26197.22634930 .00084711 00000-0 52094-3 0 9997
2 60508 97.3709 292.2964 0004998 182.2773 177.8471 15.76964238107509
Epoch: Jul 16, 2026 •
Age: 9 hours
Current Status
Altitude 362.2 km
Apogee / Perigee N/A
Velocity 7.69 km/s
Sub-Earth Point -55.17°S,
153.9°E
Launch Date Aug 16, 2024
Age 1.9 years
Type other
Technical Details
Classification Payload
Mass 55.00 kg
Dry Mass 55.00 kg
Total Mass 55.00 kg
Length 0.90 m
Diameter 0.50 m
Span 1.50 m
Shape Box + 2 pan
Manufacturer CREO
Bus Type HyperSat
Phase Status In Orbit
Owner/State CREO/PL
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