How to Calculate Time since Periapsis in Hyperbolic Orbit given Hyperbolic Eccentric Anomaly?
Time since Periapsis in Hyperbolic Orbit given Hyperbolic Eccentric Anomaly calculator uses Time since Periapsis = Angular Momentum of Orbit^3/([GM.Earth]^2*(Eccentricity of Hyperbolic Orbit^2-1)^(3/2))*(Eccentricity of Hyperbolic Orbit*sinh(Eccentric Anomaly in Hyperbolic Orbit)-Eccentric Anomaly in Hyperbolic Orbit) to calculate the Time since Periapsis, The Time Since Periapsis in Hyperbolic Orbit given Hyperbolic Eccentric Anomaly formula is defined as time that has elapsed since an object in a hyperbolic orbit passed through periapsis (the point of closest approach to the central body) based on the eccentric anomaly. Time since Periapsis is denoted by t symbol.
How to calculate Time since Periapsis in Hyperbolic Orbit given Hyperbolic Eccentric Anomaly using this online calculator? To use this online calculator for Time since Periapsis in Hyperbolic Orbit given Hyperbolic Eccentric Anomaly, enter Angular Momentum of Orbit (h), Eccentricity of Hyperbolic Orbit (e_{h}) & Eccentric Anomaly in Hyperbolic Orbit (F) and hit the calculate button. Here is how the Time since Periapsis in Hyperbolic Orbit given Hyperbolic Eccentric Anomaly calculation can be explained with given input values -> 10922.04 = 65750000000^3/([GM.Earth]^2*(1.339^2-1)^(3/2))*(1.339*sinh(2.3)-2.3).