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 a parameter used to describe the position of an object in a hyperbolic orbit relative to its central body, it's similar to the concept of eccentric anomaly used in elliptical orbits, but adapted for hyperbolic trajectories, given the eccentricity and the true anomaly of the hyperbolic orbit, the hyperbolic eccentric anomaly can be calculated using a hyperbolic analog of Kepler's equation. 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 -> 3908.76 = 2*atanh(sqrt((1.339-1)/(1.339+1))*tan(1.90240888467346/2)).