How to calculate the speed of a satellite around the sun.

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Discussion Overview

The discussion centers around calculating the speed of a satellite orbiting the sun, particularly focusing on the application of different formulas related to orbital mechanics. Participants are exploring the calculations involved and addressing issues with unit conversions and formula accuracy.

Discussion Character

  • Technical explanation
  • Mathematical reasoning
  • Debate/contested

Main Points Raised

  • One participant presents two formulas for calculating orbital speed, noting discrepancies in the results obtained from each.
  • Another participant requests clarification on the specific equation being used, indicating a lack of familiarity with orbital mechanics.
  • Participants share links to external resources that outline the equations and parameters involved in satellite motion.
  • There is a suggestion that a missing pair of brackets in the equation may lead to incorrect calculations.
  • A participant mentions a potential calculation error if an incorrect operation (squaring instead of taking the square root) is performed.
  • One participant provides a rough estimate using SI units to help contextualize the expected order of magnitude for the speed calculation.

Areas of Agreement / Disagreement

Participants do not reach a consensus on the correct application of the formulas or the resulting calculations, indicating multiple competing views and unresolved issues regarding the calculations and unit conversions.

Contextual Notes

There are limitations regarding the clarity of the equations used, potential errors in calculations, and the need for proper unit conversions that remain unresolved.

Francis Forget
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Hi guys,
I'm currently doing a little project an I need to calculate the speed of a satellite around the sun! I'm currently trying with the Earth, but i have some problem.
When I'm using this formula : (2*Pi*a*Sqrt(1-e2))/T(1±e)
I get an answer in km/s which seams pretty good. (29,75 km/s)
But when I'm using this one : Sqrt(G*M*(2/r)-(1/a)) I'm getting 1,32*1017
I don't really know how I can transform that answer into something in km/s

If I'm not clear enough, feel free to ask me questions!

Thanks!
 
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Drakkith said:
I'm not too familiar with orbital mechanics. Could you tell me what equation you're using here?

Yeah, I'm using the equation listed above but I'm going to link you different image where it's clearly listed ! Thank you very much for helping me !

Eq1 : http://i.imgur.com/GYaHMLJ.png
Where Vp is Speed,
a is the length of the semi-major axis of the elliptical orbit
e is the eccentricity
Eq2 : http://upload.wikimedia.org/math/6/6/d/66dd08fa58f176503e2f0b6603769f4d.png
Where V is Speed,
μ is the standard gravitational parameter,
r is the distance at which the speed is to be calculated
a is the length of the semi-major axis of the elliptical orbit
Image 3 : http://i.imgur.com/zzmlLKQ.png
Here is my project so far, as you can see, my answers aren't good when it comes to the second equation!
 
Last edited:
Bandersnatch said:
Is that the actual equation you're using? You missed a pair of brackets there.
Should be:
##\sqrt{GM(2/r-1/a)}##
see here:
http://en.wikipedia.org/wiki/Orbital_speed#Precise_orbital_speed
Thanks you ! But it's worse now... I'm getting :
upload_2015-4-2_16-30-38.png

What's the unit of this? How can I convert it to km/s ?

Thanks!
 
See the wikipedia link. They do the exact same calculation you're doing as an example, with numbers and units. The ##\mu## in their equation is just the same as ##GM##.
 
If you get 1016 it is a calculation error. Do you square the product instead of taking the square root?

Quick estimate using SI units: G is 10-10, M is 1030 , r and a are 1011 so 2/r is 10-11 and 1/a is half that value.
That means the product is about 108 and the square root is 10000 with units m/s, or 10km/s - which is the right order of magnitude.
 

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