An Analytical Method for Calculating Short-Term Space Interception Probability

Table 1

Initial orbital parameters of the target and interceptor.

Orbital parameter	Target orbit	Interceptor orbit
Semimajor axis	16545	36834.9
Eccentricity	0.4	0.676229
Orbit inclination	63	114.433
RAAN	25	191.606
Argument of perigee	20	111.057
Initial true anomaly	30	287.59