Calculate the Eccentricity of Gravitationally Bound Orbit
Energy
Angular Momentum
Orbiting Mass
Coefficient of Inverse Square Law
Eccentricity: {{eccentricityBoundOrbitResult()}}

Formula:

e = (1 + (2EJ2) / (mα2))12

Where,

e = Eccentricity

E = Energy

J = Angular Momentum

m = Orbiting Mass

α = GMm (Gravitation)