What Causes the Discrepancy in Doppler Shift for Satellites in Orbit?

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SUMMARY

The discussion centers on the discrepancies in Doppler shift calculations for satellites in orbit, specifically addressing a satellite at 800 km altitude. Participants calculated the satellite's relative velocity as 6720 m/s, while the expected orbital speed is 7453 m/s. The difference in values, which participants initially thought should be around 465 m/s due to Earth's rotation, turned out to be nearly double. Key calculations involved using the formula for relative velocity and considering the angle between the satellite and the receiver on the ground.

PREREQUISITES
  • Understanding of Doppler shift principles in satellite communications
  • Familiarity with orbital mechanics and satellite velocity calculations
  • Knowledge of trigonometric functions and their application in relative motion
  • Proficiency in using formulas for relative velocity and orbital speed
NEXT STEPS
  • Study the derivation of the Doppler shift formula: v = -Δf c / f0
  • Explore orbital mechanics, focusing on the calculation of orbital speed using v = √(GM / (R + h))
  • Investigate the effects of receiver position on Doppler shift measurements
  • Learn about the impact of Earth's rotation on satellite communication frequencies
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Amateur radio operators, satellite communication engineers, and students of physics interested in understanding Doppler effects in satellite transmissions.

pan Hole
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At page http://www.qsl.net/vk3jed/doppler.html" is discussed Doppler shift at various ham radio frequencies. I calculated for this Doppler shift relative velocity of their satellite as 6720 m/s. Their satellite in height of 800 km above ground and at circular orbit should have velocity of 7453 m/s (orbital speed). I thought that difference between these two values should be max 465 m/s (rotation of Earth at equator), but it is almost twice as much... Any ideas?
 
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The 6720m/s will be the maximum velocity of the satellite relative to the receiver on ground. You have to consider the angle between satellite and receiver direction.

For a satellite at horizon the relative velocity(neglecting Earth rotation) would be 7453*cos(pi/2-asin(6378/(6378+800)))=6622.
 
log0 said:
The 6720m/s will be the maximum velocity of the satellite relative to the receiver on ground. You have to consider the angle between satellite and receiver direction.

For a satellite at horizon the relative velocity(neglecting Earth rotation) would be 7453*cos(pi/2-asin(6378/(6378+800)))=6622.

He said their answer is bigger, not smaller, so the effect you mention is probably not what is causing the difference.
 
pan Hole said:
At page http://www.qsl.net/vk3jed/doppler.html" is discussed Doppler shift at various ham radio frequencies. I calculated for this Doppler shift relative velocity of their satellite as 6720 m/s. Their satellite in height of 800 km above ground and at circular orbit should have velocity of 7453 m/s (orbital speed). I thought that difference between these two values should be max 465 m/s (rotation of Earth at equator), but it is almost twice as much... Any ideas?

I get numbers close to yours. So if you add the two velocities, you get close to 7900m/s. Which band number are you using to say that they get twice the shift?
 
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berkeman said:
I get numbers close to yours. So if you add the two velocities, you get close to 7900m/s. Which band number are you using to say that they get twice the shift?

For any frequency in Table 1 I got same relative velocity -6718 m/s caluclated this way:

v = - \frac{\Delta f c}{f_0}

For orbital speed:

v = \sqrt{ \frac{G M}{ R + h }}

at altitude of 800 km i got 7466 m/s. Difference is 748 m/s. That means, I didn't get twice the shift, from shift which I suppose is correct I got twice the velocity.
 
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OK. Let's try it again. The speed the OP has calculated(6718 m/s) is the maximum relative speed between the satellite and the receiver, not the orbital speed of the satellite(7453 m/s).

The satellite is never moving directly towards the receiver on ground. There is a height difference of 800km between both. You have to consider receiver position and velocity relative to the orbit.

The example calculation I have offered has been for the most simple case I can think of. Having a fixed receiver placed in the orbit plane and the satellite passing the horizon. A satellite passing the zenith would have a relative speed of 0 m/s.
 
log0 said:
OK. Let's try it again. The speed the OP has calculated(6718 m/s) is the maximum relative speed between the satellite and the receiver, not the orbital speed of the satellite(7453 m/s).

The satellite is never moving directly towards the receiver on ground. There is a height difference of 800km between both. You have to consider receiver position and velocity relative to the orbit.

The example calculation I have offered has been for the most simple case I can think of. Having a fixed receiver placed in the orbit plane and the satellite passing the horizon. A satellite passing the zenith would have a relative speed of 0 m/s.

I am starting to understand the problem... Orbital velocity is calculated fot Earths centre and receiver is 6378 km from that centre, right? But I still don't see the way to calculation you posted...
 
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Here is a sketch. :)
 

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Thank you very much, now I understand it. I plotted Doppler shifts calculated from your formula and I got exactly same graphs as showed on that webpage.
 

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