A $5,000$ kg satellite is orbiting the Earth in a circular path. The height of the satellite above the surface of the Earth is $800$ km$.$ The velocity of the satellite is $($Me $=5\mathrm{.}981024$ kg$,$ Re $=6\mathrm{.}37106$ m$,$ G $=6\mathrm{.}6710-11$ N$$m$2/$kg$2)$

$7,460$ m$/$s$.$

$6,830$ m$/$s$.$

$6,430$ m$/$s$.$

$5,950$ m$/$s$.$

$5,350$ m$/$s$.$