True Anomaly, `nu`[E]

Not Reviewed
Equation / Last modified by KurtHeckman on 2017/10/13 13:55
Rating
ID
MichaelBartmess.True Anomaly, `nu`[E]
UUID
94fa3b89-e5d5-11e3-b7aa-bc764e2038f2

The True Anomaly calculator computes the True Anomaly (ν) of an orbit from the inputs:

True Anomaly (ν): The True Anomaly is the angle between the direction of periapsis and the current position of the body.

TrueAnomalynuE-illustration.png