Spacecraft Inertia (Principal Axes)
kg·m²
kg·m²
kg·m²
Rectangular Cuboid Shape
m
m
m
Control type
Actuator settings will appear here.
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
YYYY-MM-DD HH:MM:SS
Keplerian orbital elements
deg
deg
deg
deg
deg
deg
Playback
×
Hz
Integration
s
unitless
unitless