Table 2. Configuration of the target and the chaser
Space station
Spacecraft
Perigee, apogee (altitude)
300 km circular
320.06 km, 513.86 km
True anomaly,
θ
60°
349.65°
Inclination,
i
40°
40.130°
RA of ascending node, Ω
20°
19.819°
Argument of perigee,
ω
0° (arbitrary)
70.662°
RA, right ascension.