1. Limited time only! Sign up for a free 30min personal tutor trial with Chegg Tutors
    Dismiss Notice
Dismiss Notice
Join Physics Forums Today!
The friendliest, high quality science and math community on the planet! Everyone who loves science is here!

Geostationary Orbit Question

  1. Oct 20, 2009 #1
    1. The problem statement, all variables and given/known data

    A 10,000 kg satellite is rbiting the earth in a geostationary orbit. The height of the satellite above the surface of the earth is ???


    2. Relevant equations

    [tex] V = \omega r [/tex]

    Newtons gravitational force equation

    Keplers third law equation

    3. The attempt at a solution

    I really don't understand how to set this problem up. Here is what I am thinking. We know the radius of the earth ( 6.37 x 10 ^6 m) so all we need to find is how much above is the satellite outside of earth. That plus the radius of the earth will give me to total radius. But what equations should I use. I don't think I know [tex] \omega [/tex] nor do I know the velocity. If I use Kepler's third law equation all I get is the distance to the geosynchronous orbit. Don't know what to do.
     
  2. jcsd
  3. Oct 20, 2009 #2

    mgb_phys

    User Avatar
    Science Advisor
    Homework Helper

    In orbit the force pulling the satelite down due to gravity is equal to the outward (centripetal force)

    So for any orbital height there is a speed you need to go at to provide enough outward force. The only special thing about GSO is that the speed is exactly that needed to go around the earth on 24hours

    This is basically what Kepler's third law says - although you need the value of the constant in this case.
     
    Last edited: Oct 20, 2009
  4. Oct 20, 2009 #3
    Yes, I kind of figured that since there was no other quantity given for time, but I still don't see or understand how we would find the radius - the height of the satellite above the earth.
     
  5. Oct 20, 2009 #4
    Kepler's law

    [tex] T^2 = [ (4pi^2) / (GM_E) ] r^3 [/tex]

    I would solve for r then?

    but I am not sure if that gives me the distance TO the satellite.
     
  6. Oct 20, 2009 #5

    mgb_phys

    User Avatar
    Science Advisor
    Homework Helper

    Correct - or you can just use:
    Force due to gravity depends on radius F = GMm/r^2
    Centripetal force depends on radius F = m w^2/r
    (M is mass of Earth, m is mass of satelite)


    Set the forces equal to each other and find the raidus
    Note that r is radius of the orbit - ie measured from the centre of the Earth, to get orbital height (above sea level) you need the raious of the Earth as well
     
  7. Oct 20, 2009 #6
    WOW

    I was making such a silly mistake.
    I was doing what I said above - using Kepler's third law - but when I solved for r I just used r as my answer. Which was not correct at all. I needed to subtract The r I got from Kepler's law from the radius of the earth to get my distance.

    Such a silly mistake

    Thanks for helping me out, much appreciated.
     
Know someone interested in this topic? Share this thread via Reddit, Google+, Twitter, or Facebook




Similar Discussions: Geostationary Orbit Question
Loading...