Epoch

This attribute specifies the orbit epoch date and time, which is used to define an Initial State or Launch Segment of a Mission Control Sequence.

Syntax

Astrogator <Satellite Object Path> SetValue <Astrogator Object Path>.Epoch <Value> <Unit>

Description

Specify the Epoch date and time. Select from the standard options for a time unit of measure.

Examples

Initial State

Astrogator */Satellite/Satellite1 SetValue MainSequence.SegmentList.Initial_State.InitialState.Epoch 86400 EpSec

Astrogator */Satellite/Satellite1 SetValue MainSequence.SegmentList.Initial_State.InitialState.Epoch "Scenario/Scenario1 Today"

Launch

Astrogator */Satellite/Satellite1 SetValue MainSequence.SegmentList.Launch.Launch.Epoch 0 EpSec

Astrogator */Satellite/Satellite1 SetValue MainSequence.SegmentList.Launch.Launch.Epoch "Scenario/Scenario1 Today"

STK Programming Interface 11.0.1