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

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Discussion Overview

The discussion revolves around the discrepancies observed in the Doppler shift calculations for satellites in orbit, particularly focusing on the relative velocities of satellites and ground receivers. Participants explore the implications of orbital speed, relative motion, and the effects of Earth's rotation on these calculations.

Discussion Character

  • Technical explanation
  • Mathematical reasoning
  • Debate/contested

Main Points Raised

  • One participant calculated a relative velocity of 6720 m/s for a satellite at 800 km altitude, while the expected orbital speed is 7453 m/s, leading to questions about the significant discrepancy.
  • Another participant noted that the 6720 m/s represents the maximum relative velocity, emphasizing the need to consider the angle between the satellite and the receiver.
  • A different participant calculated the relative velocity at the horizon to be approximately 6622 m/s, suggesting that the initial claim of a larger discrepancy might not be due to the angle effect mentioned.
  • Some participants discussed adding velocities to arrive at a total of around 7900 m/s, questioning the basis for claims of a doubled Doppler shift.
  • One participant presented a formula for calculating relative velocity based on frequency shifts, indicating a difference of 748 m/s at 800 km altitude, but clarified that this does not imply a doubling of the shift.
  • Another participant reiterated that the maximum relative speed calculated does not equate to the orbital speed, highlighting the importance of considering the receiver's position and velocity.
  • One participant expressed a growing understanding of the problem and confirmed that their plotted Doppler shifts matched those shown on a referenced webpage.

Areas of Agreement / Disagreement

Participants do not appear to reach a consensus on the cause of the discrepancies in Doppler shift calculations, with multiple competing views and interpretations of the data and calculations presented.

Contextual Notes

Participants noted the importance of considering the height difference between the satellite and the receiver, as well as the angle of approach, which complicates the calculations. There are unresolved mathematical steps and assumptions regarding the definitions of velocities and shifts.

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:

[tex]v = - \frac{\Delta f c}{f_0}[/tex]

For orbital speed:

[tex]v = \sqrt{ \frac{G M}{ R + h }}[/tex]

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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