Spacecraft.NoradEquinoctialLongitude Property

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Description

This property has been Deprecated. Please use the SGP4.EquinoctialLongitude property instead.

Equinoctial Norad based Longitude defined by the mean longitude, defined as: RAAN + w + MA, where RAAN and w are the Right Ascension of the Ascending Node and the Argument of Perigee, respectively, and MA is the Keplerian mean anomaly. These orbit properties are with respect to the True Equator Mean Equinox coordinate frame.

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:	136.889123546261
Valid Range:	0 ≤ Spacecraft.NoradEquinoctialLongitude ≤ 360

Syntax

myVariable1 = mySpacecraft1.NoradEquinoctialLongitude;

mySpacecraft1.NoradEquinoctialLongitude = myVariable1;