Generic Model of a Satellite Attitude Control System

Table 2

Initial satellite orbital parameters.

Description	Value	Unit
Semimajor axis	6371 000	[m]
Eccentricity	0	[-]
Longitude of ascending node	331.7739	[°]
Orbit inclination	51.6393	[°]
Argument of perigee	0	[°]
True anomaly	20.5285	[°]
Orbital period	5500	s