The velocity ($V_s$) of a satellite moving in a circular orbit at a height of 1000 km above earth surface is ___________ km s$^{-1}$ (rounded off to 2 decimal places).
{($G = 6.67 \times 10^{-11}$ m$^3$ kg$^{-1}$ s$^{-2}$, $M_e = 5.972 \times 10^{24}$ kg and $r_e = 6378$ km)}