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# True Anomaly, `nu`[E]

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Equation / Last modified by KurtHeckman on 2017/10/13 13:55
`nu = `

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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:

- E - the eccentricity anomaly
- e - eccentricity

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

This equation,

**True Anomaly, `nu`[E]**, references 1 equation/constant.**Equations and Constants **

This equation,

**True Anomaly, `nu`[E]**, is used in 1 calculator.**Calculators**