Find the Ek of a satilite in orbit

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To find the kinetic energy (Ek) of a satellite in orbit using its mass and gravitational acceleration, one must equate the gravitational force with the centripetal force. The relationship involves using Newton's law of gravitation, F = Gmm/r², and the centripetal acceleration formula, a = v²/R. The radius (R) can be derived from R = √(GMearth/a), allowing for the calculation of velocity and subsequently the kinetic energy using Ek = 1/2 mv². The discussion emphasizes the importance of understanding each step in the calculation process to ensure comprehension. Ultimately, mastering these concepts is crucial for solving orbital mechanics problems effectively.
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How do you find the Ek of a satilite in orbit with only its mass and acceleration due to gravity?

I did something like..

Fc = Fg
mv²/r = mg <-- g = the acceleration due to gravity

but then i don't have a radius...

How do i solve this?
 
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Edit: After reading more carefully, you'll need to equate Newton's expression for gravitational force with the given mg force to determine the radius.

--J
 
Mind elaborating on that?
 
F = Gmm/r² ?
 
Yup.

--J

blah blah blah post too short my--
 
I keep getting Ek = 7.44x10^10 but its 2.99x10^9

?
 
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Did you do this?

a = \frac{v^2}{R} \Rightarrow v^2 = aR

R = ?

F = ma \Rightarrow \frac{GM_{earth}m}{R^2} = ma \Rightarrow R = \sqrt{\frac{GM_{earth}}{a}}

\Rightarrow E_k = \frac{1}{2}ma\sqrt{\frac{GM_{earth}}{a}}
 
Ah now i get it! Thanks for actually showing the steps it really helps lol.
 
No problem. I guess it's okay for me to show you the steps after you've tried to do the problem on your own. But please make sure you understand each of these steps perfectly, otherwise you're not getting out smarter out of this.
 
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