Adaptively Random Weighted Cubature Kalman Filter for Nonlinear Systems

Table 1

The orbit parameters of the spacecraft.

Orbit Parameters	Value
Semi-major axis	6865.112418km
Eccentricity	0.001248
Orbit inclination	29.059°
Right ascension of ascending node	338.82°
Argument of perigee	351.167°
True anomaly	229.46°
Orbit cycle	50076s