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True anomalyIn astronomy, the true anomaly (, also written ) is the angle between the direction ''z-s'' of periapsis and the current position ''p'' of an object on its orbit, measured at the focus ''s'' of the ellipse (the point around which the object orbits). In the diagram below, true anomaly is the angle ''z-s-p''. ==Calculation from state vectors== For elliptic orbits true anomaly can be calculated from orbital state vectors as: : (if then replace ''T'' by 2π − ''T'') where: * is orbital velocity vector of the orbiting body, * is eccentricity vector, * is orbital position vector (segment ''sp'') of the orbiting body. : ---- For circular orbits this can be simplified to: : (if then replace ''T'' by 2π − ''T'') where: * is vector pointing towards the ascending node (i.e. the z-component of is zero). : ---- For circular orbits with the inclination of zero this can be simplified further to: : (if then replace ''T'' by 2π − ''T'') where: * is x-component of orbital position vector , * is x-component of orbital velocity vector . ==Other relations== The relation between ''T'' and ''E'', the eccentric anomaly, is: : or equivalently : The relations between the radius (position vector magnitude) and the anomalies are: : and : where ''a'' is the orbit's semi-major axis (segment ''cz''). ==See also== * Kepler's laws of planetary motion * Eccentric anomaly * Mean anomaly Astrodynamics Celestial mechanics See other meanings of words starting from letter: TTA | TB | TC | TD | TE | TF | TG | TH | TI | TJ | TK | TL | TŁ | TM | TN | TO | TP | TR | TS | TU | TW | TX | TY | TZ |Words begining with True_anomaly: True_anomaly |
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