Estimating Mass of Central Object Using S2's Orbit Motion and Kepler's 3rd Law

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SUMMARY

The discussion focuses on estimating the mass of a central object using the orbit motion of star S2 and Kepler's 3rd Law. Participants clarify that the radius used in calculations is half the semi-major axis of the elliptical orbit, with an estimated value of 0.1 arcseconds for S2's orbit. The importance of correcting for orbital tilt is emphasized, as it affects the accuracy of mass estimation. The discussion references specific tools and concepts, including the arcsec relation and the need to analyze the tilt of the orbit.

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I want to understand how one can go about estimating the mass of a central object given the a graph the orbital motion of S2, or any given star for that matter.
During one of my class lectures, we were shown a graph of star S2's orbit motion (shown at the bottom of this post) and was told to try and figure out how to find the mass of the central object using Kepler’s 3rd law in solar units, as shown below:
1678026251763.png


We were also given a hint to use the arcsec relation and read the radius of the orbit from the image, as shown below:
1678026338495.png


From my notes, it looks like we had to use the declination value of 0.1, but I still don't understand how exactly we got to that point. Does anyone happen to know why this is and how to generally use these types of graphs to estimate the mass of a central object?

1678026170065.png
 
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The "radius" in the formula is actually half the semi-major axis of the ellipse (which obviously doesn't have a constant radius). Based on the diagram, 0.1'' might be a good estimate for the semi-major axis.
 
As @pasmith said, reading from the diagram, the semimajor axis is about 0.1". This is the θ in your second formula. It is not a declination, it is the angular size of the orbit.
 

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