How High Is a Geostationary Satellite Above Earth?

AI Thread Summary
The height of a geostationary satellite from the Earth's center is calculated to be approximately 2.16 billion meters. The correct orbital period for a geostationary satellite is 86400 seconds, matching the Earth's rotation period. This synchronization allows the satellite to remain fixed over a specific geographical location. There is a distinction between geostationary and synchronous satellites, though they often share similar characteristics. For detailed calculations and explanations, additional resources are available online.
crosbykins
Messages
50
Reaction score
0

Homework Statement



What is the height of a geostationary satellite measured from the Earth's centre?

Homework Equations



r^3/T^2 = GM/4pi^2

T of Earth = 3.16 * 10^7 s

The Attempt at a Solution



GM/4p2 = r3/T2
3root[T2 * GM/4p2 ] = r
3root[(3.16*107 s)2 * ((6.67*10^ -11N * m2 /kg2 )(5.98*1024 kg)/4p2 )] = r
2.16*109m = r
Therefore the height of the satellite from the Earth’s center is 2.16*109m.
 
Physics news on Phys.org
Why are you using a year as the period of the satellite?
 
gneill said:
Why are you using a year as the period of the satellite?

because in my textbook it gives 3.16*10^7 s as the period of revolution of orbit for earth, so since the satellite is geocentric its period is the same
 
A geostationary satellite has an orbit that keeps pace with the rotation of the Earth -- a daily rotation -- so that it remains over the same geographical location.
 
gneill said:
A geostationary satellite has an orbit that keeps pace with the rotation of the Earth -- a daily rotation -- so that it remains over the same geographical location.

ok well then i don't mean geocentric i just mean that it has the same orbit period as the Earth
 
Dude, your calculations are fine you are using the wrong period T.
Geostationary orbit means when you look up from Earth it appears the satellite isn't moving.
For this to be the case, the satellite must revolve around Earth at the same period as Earth rotates about it's axis.
This period is 24 hours x 60 minutes x 60 seconds = 86400 seconds.
T = 86400 seconds.
 
Jonnyb42 said:
Dude, your calculations are fine you are using the wrong period T.
Geostationary orbit means when you look up from Earth it appears the satellite isn't moving.
For this to be the case, the satellite must revolve around Earth at the same period as Earth rotates about it's axis.
This period is 24 hours x 60 minutes x 60 seconds = 86400 seconds.
T = 86400 seconds.

the question calls it a synchronous satellite...is this the same thing
 
I think you'd be better putting such a satellite at one of the http://en.wikipedia.org/wiki/Lagrangian_point" .
 
Last edited by a moderator:
Hi there,

For a full explanation of how to calculate the height of a geostationary satellite, check out a blog post I wrote on this very subject:

http://davechessgames.blogspot.com/2011/01/maths-problems-5-geostationary.html

This uses the formulae and the constants you've been given - it also calculates the distance from the centre of the Earth to the satellite, and also from the Earth's surface to the satellite.

Any problems, leave me a comment on the blog!

Cheers

Dave
 
Back
Top