Loosely Formation-Displaced Geostationary Orbit Optimization with Complex Hybrid Sail Propulsion

Table 4

Mass consumption for all spacecrafts after one day.

Time	Strict formation with ideal displaced GEO (kg)	Loosely formation with a station-keeping box (kg)	Mass saving (%)
Winter solstice	2.805	1.686	39.89%
Spring equinox	3.022	1.747	42.19%
Summer solstice	2.808	1.638	41.67%
Autumn equinox	3.021	1.751	42.04%