OperationalISROFirst Launch: 2010-04-15
GSLV Mark II
India's medium-lift launcher featuring an indigenous cryogenic upper stage, used for heavier GTO and LEO payloads than the PSLV.
SpaceStats Reliability & Flight Record
TOTAL LAUNCHES
18
Orbital missions
SUCCESSFUL
12
4 failures
SUCCESS RATE
66.7%
LANDINGS
0
Expendable Vehicle
ISROFeatured Photography
GSLV-F10 Liftoff with EOS-03
ISRO
Technical & Propulsion Specifications
Operator: ISROVehicle Dimensions & Mass
- Overall Height
- 49.13 m
- Body Diameter
- 2.8 m
- Gross Lift-off Mass
- 414.8 t
- Stages Count
- 3
- Fairing Diameter
- 3.4 m
Stage 1 (Booster)
- Recovery Mode
- Expendable
Stage 2 & Capacities
- LEO Capacity
- 6 t
- GTO Capacity
- 2.5 t
- Cost per Launch
- $47,000,000
- LEO Price / kg
- ~$7,833 / kg
Fleet Deployment & Economics Suite
Model Satellite Constellations or Payload Charters with GSLV Mark II
Calculate multi-plane Walker Delta fleet costs, fairing dispenser limits, launch cadence timelines, and single-mission rideshare economics.
High-Resolution Photo Gallery & Media
2 photos & renders of GSLV Mark II
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Liftoff2021-08-12GSLV-F10 Liftoff with EOS-03
ISRO GSLV Mk II rocket with indigenous cryogenic upper stage launching from Sriharikota.
ISRO
Source 
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Pad2018-03-26GSLV Mk II on Second Launch Pad Sriharikota
GSLV Mk II on its Mobile Launch Pedestal ready for communication satellite launch into geostationary transfer orbit.
ISRO
Source SpaceStats Launch Manifest & Database
0 mission records cataloged in database
No individual manifest entries logged in database for GSLV Mark II.
Summary stats and flight achievements are detailed in the overview above.