What is Elliptic Orbit ?
An elliptical orbit is a type of orbit in celestial mechanics where an object, such as a satellite or a planet, follows a path that is elliptical in shape around another body, such as a star or a planet. In an elliptical orbit, the object moves in a closed path around the central body, with the central body located at one of the two foci of the ellipse.
How to Calculate Radial Velocity in Elliptic Orbit given True Anomaly, Eccentricity, and Angular Momentum?
Radial Velocity in Elliptic Orbit given True Anomaly, Eccentricity, and Angular Momentum calculator uses Radial Velocity of Satellite = [GM.Earth]*Eccentricity of Elliptical Orbit*sin(True Anomaly in Elliptical Orbit)/Angular Momentum of Elliptic Orbit to calculate the Radial Velocity of Satellite, Radial Velocity in Elliptic Orbit given True Anomaly, Eccentricity, and Angular Momentum formula is defined as a measure of the velocity of an object in an elliptical orbit around a central body, providing insight into the object's motion and position in the orbit. Radial Velocity of Satellite is denoted by vr symbol.
How to calculate Radial Velocity in Elliptic Orbit given True Anomaly, Eccentricity, and Angular Momentum using this online calculator? To use this online calculator for Radial Velocity in Elliptic Orbit given True Anomaly, Eccentricity, and Angular Momentum, enter Eccentricity of Elliptical Orbit (ee), True Anomaly in Elliptical Orbit (θe) & Angular Momentum of Elliptic Orbit (he) and hit the calculate button. Here is how the Radial Velocity in Elliptic Orbit given True Anomaly, Eccentricity, and Angular Momentum calculation can be explained with given input values -> 0.002567 = [GM.Earth]*0.6*sin(2.3581143523691)/65750000000.