Geosynchronus Sattelite Question

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Homework Statement



A satellite that stays over the same spot on a planet as it rotates is called a geostationary satellite. (Geostationary satellites must be positioned somewhere over the equator of the planet.) What is the average orbital radius of a geostationary satellite for a planet with a mass of 4.82 x 10^24 kilograms and a period of rotation of 14.0 hours?

Homework Equations


The Attempt at a Solution



F = ma
Fg = GM1m2/r^2
Gm1m2/r^2 = m2(v^2/r)
GM1/r = V^2
GM1/r = (2(pi)/T)^2
GM1/r = 4(pi)^2r^2/T^2
GM1T^2/4(pi)^2 = r^3
r = approx 1.26E8 m

but i am getting it wrong
 
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cepheid said:
Looks like a computation error? I get a different answer using that same formula with those same numbers.

its 10^24... see my post again i edited the question to include the ^

edit... i got 3.34E8 now...

nvm back to 1.26E8
 
cepheid said:
Yeah, I assumed that's what it meant, but I still got a different answer from you.

hrm so

(6.67E-11) * (4.82 x 10^24) * (14*60*60)^2
/
(4(pi)^2)

so doing the math i get approx
2.01E24 ish

then do the third square root of that to get r...
and i get 1.26E8
 
bleedblue1234 said:
hrm so

(6.67E-11) * (4.82 x 10^24) * (14*60*60)^2
/
(4(pi)^2)

so doing the math i get approx
2.01E24 ish


I get approx. 2.06e22.

bleedblue1234 said:
then do the third square root of that to get r...
and i get 1.26E8

Do you mean the cube root?

It looks like there could be at least two problems with your calculation...
 
cepheid said:
I get approx. 2.06e22.
Do you mean the cube root?

It looks like there could be at least two problems with your calculation...

yes... i meant the cube root

but i am doing the calculation right and i keep getting 2.014E24

(are you doing 14*60*60 to convert hours to seconds?)
 
cepheid said:
Yes, that's about what I got.

about or is... i have 1 submission to get it right... :-p

thanks

edit: nailed the problem, much thanks