Calculate the Eccentricity of Gravitationally Bound Orbit | |
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Energy | |

Angular Momentum | |

Orbiting Mass | |

Coefficient of Inverse Square Law | |

Eccentricity: | {{eccentricityBoundOrbitResult()}} |

## Formula:

### e = (1 + (2EJ2) / (mα2))1/2

Where,

e = Eccentricity

E = Energy

J = Angular Momentum

m = Orbiting Mass

α = GMm (Gravitation)