Calculate Apocentre of Gravitationally Bound Orbital Motion | |
---|---|

Semi Latus Rectum | |

Eccentricity | |

Apocentre Distance: | {{orbitApocentreResult() | number:4}} |

## Formula:

### rmax = ro / (1-e)

Where,

rmax = Apocentre Distance of Gravitationally Bound Orbital Motion

ro = Semi Latus Rectum

e = Eccentricity