PSLV (Polar Satellite Launch Vehicle), is an expendable launch system developed and operated by the Indian Space Research Organisation (ISRO),

As you asking I am telling PSLV C23 launched the 5 foreign satellites in 2014:

ISRO PSLV (Polar Satellite Launch Vehicle), summary

Function Medium lift launch system
Manufacturer ISRO
Country of origin India
Cost per launch PSLV-CA 90 crore($15M)
Size
Height 44 metres (144 ft)
Diameter 2.8 metres (9 ft 2 in)
Mass PSLV-G: 295,000 kg (650,000 lb)
PSLV-CA: 230,000 kg (510,000 lb)
PSLV-XL: 320,000 kg (710,000 lb)
Stages 4
Capacity
Payload to LEO 3,250 kg (7,170 lb)
Payload to SSO(600 km) 1,750 kg (3,860 lb)
Payload to Sub-GTO/GTO 1,425 kg (3,142 lb)
Launch history
Status Active
Launch sites Sriharikota
Total launches 34
PSLV-G: 11
PSLV-CA: 11
PSLV-XL: 12
Successes 32
PSLV-G: 9
PSLV-CA: 11
PSLV-XL: 12
Failures 1 (PSLV-G)
Partial failures 1 (PSLV-G)
First flight PSLV: 20 September 1993
PSLV-CA: 23 April 2007
PSLV-XL: 22 October 2008
Notable payloads Chandrayaan-1, Mars Orbiter Mission, Astrosat
Boosters (PSLV-G) - S9
No boosters 6
Thrust 510 kN (110,000 lbf)
Specific impulse 262 s (2.57 km/s)
Burn time 44 seconds
Fuel Hydroxyl-terminated polybutadiene
Boosters (PSLV-XL) - S12
No boosters 6
Thrust 719 kN (162,000 lbf)
Specific impulse 262 s (2.57 km/s)
Burn time 49 seconds
Fuel Hydroxyl-terminated polybutadiene
First stage
Propellant mass 138,000 kg (304,000 lb)
Motor S139
Thrust 4,800 kN (1,100,000 lbf)
Specific impulse 237 s (2.32 km/s) (sea level)
269 s (2.64 km/s) (vacuum)
Burn time 105 seconds
Fuel HTPB
Second stage
Engines 1 Vikas
Thrust 799 kN (180,000 lbf)
Specific impulse 293 s (2.87 km/s)
Burn time 158 seconds
Fuel N2O4/UDMH
Third stage
Motor HPS3
Thrust 240 kN (54,000 lbf)
Specific impulse 295 s (2.89 km/s)
Burn time 83 seconds
Fuel HTPB
Fourth stage
Engines 2 x L-2-5
Thrust 15.2 kN (3,400 lbf)
Specific impulse 308 s (3.02 km/s)
Burn time 425 seconds
Fuel MMH/MON