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 millisecond timing precision mode.

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

 

Attributes

Type:

number

Access:

read

Units:

km2/s2

 

Syntax

myVariable1 = mySpacecraft1.Energy;

 

See also

Spacecraft Object

Spacecraft Propagation Guide

Coverage and Contact Analysis Guide