Spacecraft.BL_Elements Property

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Description

Represents the instantaneous Spacecraft orbital state as Brouwer-Lyddane Mean Keplerian elements. The Spacecraft state is reported as the following mean element set semi-major axis, eccentricity, inclination, right ascension of ascending node, argument of perigee, and mean anomaly.

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:	Array of number (size = 6)
Access:	read/write

Syntax

myVariable1 = mySpacecraft1.BL_Elements[0];

mySpacecraft1.BL_Elements[0] = myVariable1;