Orbital state vectors
Cartesian vectors of position and velocity of an orbiting body in space / From Wikipedia, the free encyclopedia
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In astrodynamics and celestial dynamics, the orbital state vectors (sometimes state vectors) of an orbit are Cartesian vectors of position () and velocity () that together with their time (epoch) () uniquely determine the trajectory of the orbiting body in space.[1]:ā154ā
Orbital state vectors come in many forms including the traditional Position-Velocity vectors, Two-line element set (TLE), and Vector Covariance Matrix (VCM).