How to Calculate Mean Anomaly in Hyperbolic Orbit given Hyperbolic Eccentric Anomaly?
Mean Anomaly in Hyperbolic Orbit given Hyperbolic Eccentric Anomaly calculator uses Mean Anomaly in Hyperbolic Orbit = Eccentricity of Hyperbolic Orbit*sinh(Eccentric Anomaly in Hyperbolic Orbit)-Eccentric Anomaly in Hyperbolic Orbit to calculate the Mean Anomaly in Hyperbolic Orbit, The Mean Anomaly in Hyperbolic Orbit given Hyperbolic Eccentric Anomaly formula is defined as angular distance covered by an object in its hyperbolic trajectory since passing through periapsis (closest point to the central body). Unlike in elliptical orbits, the Mean Anomaly in a hyperbolic orbit is not directly proportional to time. Mean Anomaly in Hyperbolic Orbit is denoted by M_{h} symbol.
How to calculate Mean Anomaly in Hyperbolic Orbit given Hyperbolic Eccentric Anomaly using this online calculator? To use this online calculator for Mean Anomaly in Hyperbolic Orbit given Hyperbolic Eccentric Anomaly, enter Eccentricity of Hyperbolic Orbit (e_{h}) & Eccentric Anomaly in Hyperbolic Orbit (F) and hit the calculate button. Here is how the Mean Anomaly in Hyperbolic Orbit given Hyperbolic Eccentric Anomaly calculation can be explained with given input values -> 4.310592 = 1.339*sinh(2.3)-2.3.