- #1
ArbazAlam
- 10
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Homework Statement
Use Kepler's Third Law and a Taylor expansion to derive the following approximation for the orbital period of a satellite in low Earth orbit with a constant height h above the surface of the Earth. h << R_earth :
[tex]P \approx P_{0}(1+3h/2R_{e})[/tex]
Homework Equations
Kepler's Third Law:
[tex]P^{2}=4\pi^{2}r^{3}/GM[/tex]
Taylor Expansion:
[tex]f(x)=\sum^{\infty}_{n=0}f^{n}(x-a)/n![/tex]
The Attempt at a Solution
I'm pretty certain my professor doesn't want us to expand the Taylor series beyond the first degree. I tried to write Kepler's Third Law in terms of just P and then write out the Taylor expansion about 0 (McLaurin series), but all terms came out to 0. I'm not 100% sure where to go beyond the definitions of Kepler's Law and the Taylor expansion.
I'm also confused why, if we are assuming h<<R_e, the variable h is even necessary.
I'm not asking for a solution, but any hints are much appreciated.
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