Spacecraft.BLJ2W Property

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Description

Mean Argument of Perigee in the J2 Brouwer Lyddane Element set, which is calculated using only the J2 zonal harmonic coefficient in the Brouwer-Lyddane conversion, and referenced to the ICRF. The Argument of Perigee is defined by the angle measured at the center of the Earth in the orbit plane, from the ascending node to perigee.

 

Timing Precision Mode

This page describes functionality in millisecond timing precision mode. Millisecond timing precision mode is deprecated and will be removed in a future release. We recommend that you migrate your Mission Plans to nanosecond timing precision mode.

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

 

Attributes

Type:

number

Access:

read/write

Units:

deg

Default Value:

48.739821649569

Valid Range:

0 ≤ Spacecraft.BLJ2W ≤ 360

 

Syntax

myVariable1 = mySpacecraft1.BLJ2W;

 

mySpacecraft1.BLJ2W = myVariable1;

 

See also

Spacecraft Object

Spacecraft Propagation Guide

Coverage and Contact Analysis Guide