How to Calculate Hyperbolic Eccentric Anomaly given Eccentricity and True Anomaly?
Hyperbolic Eccentric Anomaly given Eccentricity and True Anomaly calculator uses Eccentric Anomaly in Hyperbolic Orbit = 2*atanh(sqrt((Eccentricity of Hyperbolic Orbit-1)/(Eccentricity of Hyperbolic Orbit+1))*tan(True Anomaly/2)) to calculate the Eccentric Anomaly in Hyperbolic Orbit, The Hyperbolic Eccentric Anomaly given Eccentricity and True Anomaly formula is defined as angle that defines the object's position within the hyperbolic orbit, given the true anomaly. Eccentric Anomaly in Hyperbolic Orbit is denoted by F symbol.
How to calculate Hyperbolic Eccentric Anomaly given Eccentricity and True Anomaly using this online calculator? To use this online calculator for Hyperbolic Eccentric Anomaly given Eccentricity and True Anomaly, enter Eccentricity of Hyperbolic Orbit (e_{h}) & True Anomaly (θ) and hit the calculate button. Here is how the Hyperbolic Eccentric Anomaly given Eccentricity and True Anomaly calculation can be explained with given input values -> 1.190676 = 2*atanh(sqrt((1.339-1)/(1.339+1))*tan(1.90240888467346/2)).