To calculate velocity of satellite,
V=√(G.M earth)/r
Where V is velocity of satellite
G= gravitational constant=6.67×10^-11 m^3kg^-1s^-2
M earth is mass of earth=5.972×10^24 kg
r is distance between satellite and earth core=6371+600=6971 km=6971000m
So V= √((6.67×10^-11)×(5.972×10^24))/6971000 =7907.13 m/s
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