Spacecraft.Energy Property

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Description

Represents the instantaneous specific energy (energy per unit mass) of the Spacecraft orbit. This is calculated based on the Keplerian gravitational potential model as Energy = -mu/(2*a).

Timing Precision Mode

This page describes functionality in nanosecond timing precision mode.

Click here to see the documentation for this object in millisecond timing precision mode.

Attributes

Type:	number
Access:	read
Units:	km2/s2

Syntax

myVariable1 = mySpacecraft1.Energy;