Spacecraft.ApogeeHeight Property

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Description

Returns the instantaneous osculating apoapsis height of the Spacecraft above its central body, measured along a vector normal to the surface of the body at the Spacecraft's sub-satellite point. The oblateness of the central body is taken into account when calculating the height.

 

Timing Precision Mode

This page describes functionality in nanosecond timing precision mode.

 

Attributes

Type:

number

Access:

read

Units:

km

 

Syntax

myVariable1 = mySpacecraft1.ApogeeHeight;

 

See also

Spacecraft Object

Spacecraft Propagation Guide

Coverage and Contact Analysis Guide