Configuration Presets
Spacecraft inertia (principal axes)
kg·m²
kg·m²
kg·m²
Spacecraft dimensions
m
m
m
Control type
Angular velocity
Body frame with respect to inertial frame, in body frame coordinates
rad/s
rad/s
rad/s
Attitude quaternion
Body frame with respect to inertial frame. Scalar component last
unitless
unitless
unitless
unitless
Date
YYYY-MM-DD HH:MM:SS
Keplerian orbital elements
km
unitless
deg
deg
deg
deg
Simulation parameters
s
Hz
x