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

• 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.