| Calculate the Eccentricity of Gravitationally Bound Orbit | |
|---|---|
| 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)
