Spacecraft.BLJ2MA Property

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Description

Mean Anomaly 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 Mean Anomaly is defined as the angle from the eccentricity vector to a position vector corresponding to the location of the satellite if it is always moved at a constant angular rate.

 

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:

146.004208326201

Valid Range:

0 ≤ Spacecraft.BLJ2MA ≤ 360

 

Syntax

myVariable1 = mySpacecraft1.BLJ2MA;

 

mySpacecraft1.BLJ2MA = myVariable1;

 

See also

Spacecraft Object

Spacecraft Propagation Guide

Coverage and Contact Analysis Guide