| Description | Ingest Orbit prediction (OEM) files into ORBIT4ANT table |
|---|---|
| Docstring | Ingester module for the Orbit Prediction state vectors file type (OEMORBPRED). This is an XML file which contains a number of , as shown below: <stateVector> <EPOCH>2020-12-01T00:00:00.000Z</EPOCH> <X>-6.780290602793E+03</X> <Y>-6.797782401015E+02</Y> <Z> 3.621533494135E+03</Z> <X_DOT>-2.654711849949E+00</X_DOT> <Y_DOT>-3.582661194453E+00</Y_DOT> <Z_DOT>-5.637075170929E+00</Z_DOT> </stateVector> |
| Wiki page | None |
| Activity file | ORBIT4ANT_INGESTER.xml |
| Executable | alg/orbit4ant_ingester.py |
| Calling convention | filename |
| Table triggers | None |
| Scheduler triggers |
|
| Output tables | None |
| Event raised | None |