Answer:
[tex]4.8 \cdot 10^4 N[/tex]
Explanation:
The force of gravity acting on the satellite is given by:
[tex]F=\frac{GMm}{r^2}[/tex]
where
G is the gravitational constant
[tex]M=5.98\cdot 10^{24} kg[/tex] is the Earth's mass
m is the mass of the satellite
r is the distance of the satellite from the Earth's centre
Here we have
m = 700 kg
[tex]r=2.4\cdot 10^6 m[/tex]
Substituting into the equation, we find:
[tex]F=\frac{(6.67\cdot 10^{-11})(5.98\cdot 10^{24})(700)}{(2.4\cdot 10^6)^2}=4.8 \cdot 10^4 N[/tex]
Note that the distance mentioned in the problem (2.4 x 10^6 meters) is not realistic, since it is less than the radius of the Earth (6.37 x 10^6 meters).