Spacecraft.BL_MA Property

Top

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 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:	267.760589838412
Valid Range:	0 ≤ Spacecraft.BL_MA ≤ 360

Syntax

myVariable1 = mySpacecraft1.BL_MA;

mySpacecraft1.BL_MA = myVariable1;