Spacecraft.LongAscendingNodeErrorKm(Variable, Variable) Method

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Description

Returns the offset of the actual ascending node on the surface of the central body from a user-defined global reference longitude grid measured at the Ascending Node. The global reference longitude grid is also referred to as a repeating groundtrack grid. The repeating groundtrack grid represents the nominal nodal longitudes the Spacecraft would fly over, spaced evenly around the equator. Note that this property is Earth-specific.

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.

Note: This method has a state. See the Methods and Properties with State page for more information.

Method Signature

Spacecraft.LongAscendingNodeErrorKm(	Variable baseLongitude,
	Variable repeatCycle)

Arguments

baseLongitude
Description:	Defines the nominal longitude reference grid for repeating at the node.
Units:	deg
Valid Range:	-360 ≤ baseLongitude ≤ 360

repeatCycle
Description:	Number of orbital revolutions the Spacecraft completes before the Spacecraft groundtrack repeats.
Valid Range:	repeatCycle ≥ 0

Return Value

Type:	number
Units:	km

Returns the offset of the actual ascending node on the surface of the central body from a user-defined global reference longitude grid measured at the Ascending Node. Note that this property is Earth-specific.

Syntax

myVariable1 = mySpacecraft1.LongAscendingNodeErrorKm(myVariable2, myVariable3);