The spacecraft shown is symmetrical about its $z$ -axis and has a radius of gyration of $720 \mathrm{mm}$ about this axis. The radii of gyration about the $x$ - and $y$ -axes through the mass center are both equal to $540 \mathrm{mm}$ When moving in space, the $z$ -axis is observed to generate a cone with a total vertex angle of $4^{\circ}$ as it precesses about the axis of total angular momentum. If the spacecraft has a spin velocity $\dot{\phi}$ about its $z$ -axis of $1.5 \mathrm{rad} / \mathrm{s}$, compute the period $\tau$ of each full precession. Is the spin vector in the positive or negative $z$ -direction?