.. default-role:: math
:sd_hide_title:
.. caution:: Under construction...beep beep beep...
Standard Orbital Elements
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:Info: **Standard Orbital Elements:** Express the particle's motion in terms of the standard set of orbital elements, `(a, e, i, \omega, \Omega, M)` for closed trajectories.
:Description: See above.
Shape `(a,e)`
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It shouldn't come as a surprise that the trajectory we've found in the orbital plane
Orientation `(i,\omega,\Omega)`
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Rotation matrix stuff to get back to the original `(X,Y,Z)` frame
Position `(M)`
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Mean anomaly, eccentric anomaly, Kepler equation