Spacecraft.BL_MA Property

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Description

Mean Anomaly of the Spacecraft referenced to the ICRF in the Brouwer-Lyddane Mean Element set. 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 always moved at a constant angular rate.

 

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:

267.760589838412

Valid Range:

0 ≤ Spacecraft.BL_MA ≤ 360

 

Syntax

myVariable1 = mySpacecraft1.BL_MA;

 

mySpacecraft1.BL_MA = myVariable1;

 

See also

Spacecraft Object

Spacecraft Propagation Guide

Coverage and Contact Analysis Guide