How Far is the Satellite from Earth?

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To determine the radius of a satellite's orbit given its gravitational force, the equation used is F = G(m1m2/d^2). A user initially calculated a distance of 40,000 km but found inconsistencies when checking the force. Another participant suggested using meters instead of kilometers for accuracy, leading to a recalculation that resulted in approximately 12,000 km. The discussion highlighted the importance of careful calculation and unit conversion in solving gravitational problems. Ultimately, the correct radius was clarified through collaborative troubleshooting and recalculating.
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Homework Statement


A 320kg satellite experiences a gravitational force 800N. What is the radius of the satellite's orbit?


Homework Equations


G m1m2 / d^2


The Attempt at a Solution


I started with

800N = (G(320kg)(5.98(10^24)kg) / d^2

After some algebra and rounding I ended up with d = 40,000 km. Is that reasonable?
 
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when I put 40,000 km into the original equation and solve for the force I get around 79.77N

what value did you use for G?
 
I think the standard for any calculations in classical mechanics is kg and meters. So perhaps if you try 40,000,000m.

I used 6.67 x 10 ^-11 for G.
 
Shameless bump. Still need help.
 
I kept trying again and again but I am getting 12k kilometers

d = \sqrt{\frac{GMm}{F}}

yes?

so d = \sqrt{\frac{(6.67*10^{-11}N*(\frac{m^{2}}{kg^{2}}))(5.98*10^{24}kg)(320kg)}{800 N}} = 1.26*10^{7} m

maybe you can point out where our calculations differ? I might be doing something hilariously incorrect.
 
No, you're right. I re-did the calculation again and paid proper attention to parenthesis this time. I'm just not calculator savvy at all.
 
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