| 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
