Spacecraft.OrbitalAngularMomentum Property

 Top 

Description

Represents the instantaneous specific orbital angular momentum (angular momentum per unit mass) vector about the central body referenced in the ICRF.

 

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:

Array of number (size = 3)

Access:

read

Units:

km2/s

 

Syntax

myVariable1 = mySpacecraft1.OrbitalAngularMomentum[0];

 

See also

Spacecraft Object

Spacecraft Propagation Guide

Coverage and Contact Analysis Guide