For a thin gyrocompass flywheel with rotational symmetry, the perpendicular axis theorem gives . This does not require the mass to be concentrated at the rim. Convert the specified spin to angular velocity and use one sidereal day for Earth's rotation:
At the given latitude,
The associated oscillation period is . This uses the stated neglect of the support assembly's contribution to the moment of inertia; a substantial additional vertical moment of inertia would lengthen the oscillation period.

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