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Geostationary Satelitte (1 Viewer)

wrxsti

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Given that the mass of the earth is 6 x 10^24 and raduis of the earth is 6370000m determine the height above the earths surface for a geostationary satelitte

i know period is 24 hours for a geostationary orbit and i know we need to use keplers law somewhere but i dont how to apply it
 

jonni

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Force(centripetal)=Force(gravity)

(mv^2)/r=(GMm)/r^2

because v=(2pi r)/T
substituting v and re-arranging:

r^3=(GMT^2)/(4pi^2)

r^3=(6.67*10^-11*6*10^24*(24*60*60)^2) / (4pi^2)

r=4.23*10^7m

from earth surface= 4.23*10^7 - 6.37*10^6
=3.59*10^7m above earth's surface
 

wrxsti

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thanks but isnt the force of gravity... g = GM/r^2 not g= GMm/r^2
(First line)
 

jonni

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g= GMm/r^2 is the force of attraction due to two bodies. ie. (Satelitte and earth)
the mass of the Satelitte(m) cancels out in the equations, leaving the mass of earth (M).
 
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xiao1985

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@jonni: correct, though I refer F = GMm/r^2

since g= gravitational acceleration usually.
 

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