Table 4. Fuel consumption in each operation phase computed from STK software

Maneuver	Fuel usage (kg)	Etc.
Rising	38.389	Altitude ~1,800 km
Propagation	0	About 6 month
Rising periapsis	0.27
Lowering apoapsis	25.993
Inc and RAAN control	12.858
Proximity	< 1	V-bar approach
Capturing	0
De-orbit	-	Electrical propulsion Natural decay at 200 km altitude
Total	78.9865

STK, Satellite Tool Kit.