Answer:
7.457 * 10³ m/s
Explanation:
Parameters given:
Mass of earth, M = 6 * 10^24 kg
Radius of orbit, R = 7.2 * 10^6 m
Orbital velocity is given as:
v = √(GM/R)
Where G = gravitational constant
v = √(6.673 * 10^(-11) * 6 * 10^24)/(7.2 * 10^6)
v = √(5.561 * 10^7)
v = 7.457 * 10³ m/s