GR & Time Dilation: Solve Satellite Orbit Problem

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Homework Help Overview

The problem involves a satellite in circular orbit around the Earth and compares the time rates of a clock on the satellite with an identical clock on Earth. It explores concepts of gravitational potential and time dilation in the context of general relativity.

Discussion Character

  • Exploratory, Conceptual clarification, Mathematical reasoning

Approaches and Questions Raised

  • Participants discuss the gravitational potential of the satellite and Earth, with attempts to calculate the difference in potential. Questions arise regarding the orbital velocity and its effect on time dilation. Some participants express confusion about the conditions under which the orbiting clock is faster.

Discussion Status

The discussion is ongoing, with participants exploring various aspects of the problem, including gravitational effects and the implications of orbital motion on time rates. Some guidance has been offered regarding the use of the Lorentz factor and approximations, but no consensus has been reached.

Contextual Notes

Participants note the specific conditions under which the orbiting clock is faster and the significance of the altitude of the satellite. There is also mention of potential confusion regarding the calculations and signs in the equations.

Lorna
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I am sorry for posting this problem again. I posted it in introductory physics and someone mensioned it might not be an introductory physics problem. Any way I still don't have an answer to it so thought of asking you all, thanks.

Homework Statement


A satellite is in circular orbit of radius r about the Earth (Radius R, mass M). Astandard clock C on the satellite is compared with an identical clock C0 at the south pole on Earth. Show that the ratio of the rate of the orbiting clock to that of the clock on Earth is approximately:

1+(GM/Rc^2)-(3GM/2rc^2).

Note that the orbiting clock is faster only if r > 3/2 R, ir if r-R>3184 km.


Homework Equations



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The formula to find the rate is : 1+delta (potential)/c^2
so I have to find the diffrence between the potential


The Attempt at a Solution



potential on Earth = -GM/R
potential of object in orbit = -GM/r

diffrence = GM/R-GM/r

answer should be : GM/R-3GM/2r --- so my answer is wrong
 
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Lorna said:

Homework Statement


A satellite is in circular orbit of radius r about the Earth (Radius R, mass M). Astandard clock C on the satellite is compared with an identical clock C0 at the south pole on Earth. Show that the ratio of the rate of the orbiting clock to that of the clock on Earth is approximately:

1+(GM/Rc^2)-(3GM/2rc^2).

Note that the orbiting clock is faster only if r > 3/2 R, ir if r-R>3184 km.

I think I smell the rat. Don't forget that the satellite is also in motion relative to the Earth's surface. What is the orbital velocity at radius r? What is the time dilation effect for that velocity (as a linear approximation)? [I thought it seemed odd that the orbiting clock was faster only above a certain altitude... Note that the standard clock is at the South Pole: what is the linear speed of the clock there?]
 
Last edited:
orbital v = (GM/r)^1/2

so do we add 1/2 m v^2 + GmM/r = 3/2 G mM/r ~ 3/2 GM/r ? and then
delta (phi) = 3/2 G M/r - GM/R? If that's correct then I missed up with the signs.
 
You don't add the terms as such. Your calculation for the ratio of "time rates" at radius r is correct (to first order). This would give you the rate for a clock stationary with respect to the Earth's center (or the clock at the South Pole).

You would now multiply this rate by the Lorentz factor, gamma, for a clock moving at the orbital velocity with respect to Earth's center. What will that factor look like? If you use the binomial approximation, what is this factor approximately? You would then multiply this binomial with the binomial approximation you have for the "gravitational" effect (and only keep the "low order" terms).
 

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