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;