Add skill: orbital-elements-to-state#76
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New Skill Submission
Skill Name: orbital-elements-to-state
Skill ID:
skp-mgk1izoiaexr9pw7ozgigy6bVersion: 1.0.0
Author: jsy96
Description
Convert six classical orbital elements to J2000 ECI state vectors position and velocity using Vallado Equation 2-73 vy=v_factor*(e+cos(nu)) with Newton iteration for Kepler equation. Use when user needs orbital mechanics coordinate transformation.
Installation
This PR was automatically generated by Refly when the skill was published.