The force of gravity between the Earth and the satellite can be calculated using the following formula:
F = G x (m1 x m2) / r^2
where F is the force of gravity, G is the gravitational constant (6.67 x 10^-11 Nm^2/kg^2), m1 is the mass of the Earth, m2 is the mass of the satellite, and r is the distance between the centers of the Earth and the satellite.
First, we need to calculate the distance between the satellite and the center of the Earth:
r = radius of the Earth + altitude of the satellite
r = 6.37 x 10^6 m + 6.5 x 10^4 m
r = 6.433 x 10^6 m
Now we can calculate the force of gravity:
F = G x (m1 x m2) / r^2
F = (6.67 x 10^-11 Nm^2/kg^2) x (5.97 x 10^24 kg x 29 kg) / (6.433 x 10^6 m)^2
F = 8.76 x 10^3 N
Therefore, the force of gravity between the Earth and the satellite is approximately 8,760 N.