OrbitStateObservationGenerator Object

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Description

The OrbitStateObservationGenerator object creates observations to use in the fit of a trajectory. The typical use case is for when generating a Norad state as part of the SGP4StateEstimator object.

 

Inheritance Hierarchy: Object->OrbitStateObservationGenerator

 

Available In Editions:

Mission

 

Timing Precision Mode

This page describes functionality in nanosecond timing precision mode.

Click here to see the documentation for this object in millisecond timing precision mode.

 

Properties

 

Methods

 

 

See also

Two-Line Element Set File

Working with TLEs and the SGP4 Propagator

SGP4StateEstimator

TLECatalog

TwoLineElement