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NORAD ID: 39768 Int'l Des: 2014-029 Owner: KASH Country: J operational
LEOCIRCULARRETROGRADESSO

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About SOCRATES

SOCRATES (NORAD 39768) is a satellite launched May 24, 2014 by KASH of J. It operates in LEO, CIRCULAR, RETROGRADE, SSO orbit with a mass of 50.00 kg.

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Altitude History

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Two-Line Element Set

1 39768U 14029C 26189.85766571 .00001656 00000-0 15742-3 0 9990
2 39768 97.9094 303.4858 0004690 265.2646 94.8038 14.94860951657641
Epoch: Jul 8, 2026 • Age: 37 hours

Current Status

Altitude 595.2 km
Apogee / Perigee N/A
Velocity 7.56 km/s
Sub-Earth Point -36.35°S, 118°W
Launch Date May 24, 2014
Age 12.1 years
Type other

Technical Details

Classification Payload
Mass 50.00 kg
Dry Mass 50.00 kg
Total Mass 50.00 kg
Length 0.51 m
Diameter 0.49 m
Span 1.39 m
Shape Box + 2 pan
Manufacturer AESCO
Bus Type Socrates
Phase Status In Orbit
Owner/State KASH/J

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