An oblate spin$-$stabilized satellite has mass m$=5000$kgt$=0$ vec$(\backslash$omega $)=0\mathrm{.}01$hat$($b$)\_(1)-0\mathrm{.}04$hat$($b$)\_(2)+0\mathrm{.}7$hat$($b$)\_(3)($ra$($d$)/($s$)).$ The satellite has radius R$=0\mathrm{.}75$m and length L$=0\mathrm{.}3$m$.$ There

is no external torque acting on the satellite. For a cylinder $($assuming uniform mass distribution$),$

the inertia values are