Introduction
============

pysatMissions allows users to run build simulated satellites for Two-Line
Elements (TLE) and add empirical data.  It includes the missions_ephem and
missions_sgp4 instrument modules which can be imported into pysat.

Main Features
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- Simulate satellite orbits from TLEs and add data from empirical models
- Import magnetic coordinates through apexpy and aacgmv2

This document covers installation, a tutorial on pysatMissions including
demonstration code, and an API reference.