Spacecraft.BLJ2Elements Property

Top

Description

Represents the instantaneous Spacecraft orbital state as Brouwer-Lyddane Mean Keplerian elements, where ONLY the J2 zonal harmonic coefficient is used in the conversion. 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 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:	Array of number (size = 6)
Access:	read/write

Syntax

myVariable1 = mySpacecraft1.BLJ2Elements[0];

mySpacecraft1.BLJ2Elements[0] = myVariable1;