Answer:
Kinetic energy of satellite will be 4.98 × 10^9 J.
Explanation:
The velocity V of a satellite orbiting around the earth is given by
V = √(GM/r) ………. (i)
Where,
G = gravitational constant = 6.67 × 10^-11 Nm^2/kg^2
M = mass of earth = 5.97 × 10^24 kg
r = radius of orbit = 8 × 10^6 m
By putting values in equation (i),
V = √((6.67 × 10^-11)(5.97 × 10^24)/ 8 × 10^6)
V = 7055.13 m/s
We know that,
Kinetic energy = ½ mV^2
Where,
m = mass of satellite
so,
Kinetic energy = ½ (200)(7055.13)^2
Kinetic energy = 4.98 × 10^9 J