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A CSC of 13500 kg mass and an autonomous SB block of 3100 kg mass with a cargo bay of 10400 kg mass for storage of liquid cargoes of up to 150 tons mass. All the system is put into orbit in two launches of the CR "Zenith-2".
With apogee altitude equal to 500 km, the speed in perigee -- 7858 m/s, with speed alterations by a value of around ±15 m/s (around 30 m/s in total).
Electric power of the membrane solar batteries (SB) -- 6,22 MW
Electric power of the fuel cells (FC) -- 3.73 MW
Electric power of electrorocket engines (ERE) -- 3.73 MW.
ERE efficiency -- 0.6
FC charging efficiency -- 0.6
ERE specific pulse 31750 m/s
SB mass -- 3100 kg (0.5 kg/KW)
FC mass -- 3700 kg (1 kg/KW)
ERE mass -- 2775 kg (0.75 kg/KW)
Cargoes' catcher mass -- 1000 kg.
The rest equipment mass -- 6025 kg.
Mass of the captured portion of cargo -- 50 kg.
Length of the track of the cargo substance -- 8000m.
Time of track capturing -- 1 s.
Acceleration of braking in course of cargo capturing -- 29.1 m/s2 (~3 g).
Number of operations on cargo capturing for 1 year -- 500.
Mass of the captured cargo for 1 year -- 250 tons.
Mass of the cargo used in ERE for 1 year -- 62.5 tons.
Mass of the cargo accumulated in the orbit for 1 year -- 187.5 tons.
The fleet of multiuse suborbital rockets for exploitation in course of 1 year -- 12-25 pieces (with 200-400 launches/rocket endurance).

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