For a satellite escape velocity is $11 \mathrm{~km} / \mathrm{s}$. If the satellite is launched at an angle of $60^{\circ}$ with the vertical, then escape velocity will be
(a) $11 \mathrm{~km} / \mathrm{s}$
(b) $11 \sqrt{3} \mathrm{~km} / \mathrm{s}$
(c) $\frac{11}{\sqrt{3}} \mathrm{~km} / \mathrm{s}$
(d) $33 \mathrm{~km} / \mathrm{s}$