Spacecraft.BL_MA Property

Top 

Description

Mean Anomaly of the Spacecraft in Mean of J2000 Earth-Equator coordinates 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;

 

See also

Spacecraft Object

Spacecraft Propagation Guide

Coverage and Contact Analysis Guide