Effect of time dilation on a satellite

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mfb said:
Correct. As Earth's gravitational field is weak you can treat both time dilation effects as independent. Add the velocity/height relation for an orbit and you can get a closed formula. Here is a graph. At 3000 km clocks run at the same speed as on the ground (for circular orbits). Below they run slower, above they run higher.

I thought I'd seen the calculation once that the ISS was high enough. Apparently not. I'll remember that. Thanks.
 
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PeroK said:
Is there a calculation for that? I would have thought that in the limit of a very large orbit, the gravitational effect would dominate. And, in the limit of a very low orbit, velocity based time dilation would dominate.
For a clock in a circular orbit , the time dilation is
$$ t_0 = t_f \sqrt{1- \frac{3GM}{r c^2}}$$
when r is the orbital radius
Ignoring effects due to the rotation of the Earth, time dilation at the Earth's surface is
$$ t_0 = t_f \sqrt{1- \frac{2GM}{r_e c^2}}$$

with re being the radius of the Earth

$$ t_f \sqrt{1- \frac{3GM}{r c^2}}= t_f \sqrt{1- \frac{2GM}{r_e c^2}}$$
when
$$ r = \frac{3}{2}r_e $$

or the altitude of the orbit is 1/2 Earth radius above the surface of the Earth.
Below that, clocks run slow compared to surface clocks, above it, they run faster.
 
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some bloke said:
but that theme has, perhaps, been over-done

Pretty much any theme has been overdone :frown: Only the telling differentiates your iteration from the others. Which is where the challenge of writing arises from, of course, so go with your idea, @some bloke, and make the telling the best it can be. That's always worth reading, no matter how common (or uncommon) the scenario is.
 
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