Respuesta :

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).

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