Research on Minimum Time Interception Problem with a Tangent Impulse under Relative Motion Models

Table 1

Initial orbit parameters of the satellite and target.

Orbital parameter	Target orbit	Satellite orbit
Semimajor axis (km)	16545.13	16535.13
Eccentricity	0.4	0.399
Orbit inclination (°)	90	90
RAAN (°)	0	0
Argument of perigee (°)	20	19.99
Initial true anomaly (°)	30	29.99