Spacecraft.I Property

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Description

The Keplerian inclination (i). The angle between the orbit plane and the fundamental plane of the Mean of J2000 Earth-Equator coordinate frame.

 

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/write

Units:

deg

Default Value:

98.2300386058543

Valid Range:

-180 ≤ Spacecraft.I ≤ 180

 

Syntax

myVariable1 = mySpacecraft1.I;

 

mySpacecraft1.I = myVariable1;

 

See also

Spacecraft Object

Spacecraft Propagation Guide

Coverage and Contact Analysis Guide