How Do Kepler's Laws Explain Satellite Orbits and Gravity Points?

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This discussion focuses on the application of Kepler's Laws to determine the orbital periods of satellites and the concept of Lagrange points in gravitational fields. Using Kepler's Third Law, the period of Satellite X, which orbits at a distance eight times greater than Satellite Y, is calculated to be 22.6 times that of Satellite Y. However, the answer key indicates a factor of 4.0, suggesting a discrepancy in the calculations. Additionally, the discussion introduces the concept of Lagrange points, where gravitational forces balance, specifically between the Earth and the Moon.

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1) Satellite X and Satellite Y orbit the earth. The distance between X and the Earth is 8 times greater than the distance between Y and the earth. Using Kepler's Laws, the period of satellite X is what factor times the period of satellite Y?

R is the distance between satellite Y and the earth

I used Kepler's third law:

T^2=R^3 for Y
T^2=(8R)^3 for X

So T for Y would be R^(3/2)
and T for X would be 22.6*R^(3/2)

So the factor is 22.6 right? But the answer key says "4.0" So am I right?

2) There is a point between the Earth and the moon where the net force of gravity on an object located at that point would be zero. I have no idea which formula to use on this problem, please help.
 
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Thank you!This is known as the Lagrange point, and it is determined by a combination of Newton's law of gravity and the equations of motion. You can find more information about it here: https://en.wikipedia.org/wiki/Lagrangian_point
 

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