Maneuver Strategy for Active Spacecraft to Avoid Space Debris and Return to the Original Orbit

Table 2

The six elements of initial moment active spacecraft and disintegrating spacecraft disintegrating moment orbit.

	Active spacecraft	Disintegrating spacecraft
Semimajor axis/km	42164	42014
Eccentricity	0	0
Inclination/°	15	60
Right ascension of the ascending node/°	0	0
Argument of perigee/°	38	245
True anomaly/°	316	142