HCW.CurrentReferenceOrbit Property

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Description

The Keplerian state of the HCW propagator's InitialReferenceOrbit when propagated using a two body (Keplerian) propagator from the InitialReferenceOrbitEpoch to the Spacecraft's current epoch. The reference orbit is specified in Keplerian elements (A, E, I, RAAN, W, TA)

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

Syntax

myVariable1 = myHCW1.CurrentReferenceOrbit[0];