describe in brief the process of launching of the chandrayaan-2 ?
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The Chandrayaan-2 mission profile starts with the GSLV MKIII launch vehicle injecting the combined stack of lunar orbiter and lander modules (wet mass ~ 3320 kg) into a Transfer Orbit. The orbiter and lander are injected to a 170 x 45,75 km transfer orbit or EPO (Earth Parking Orbit) by the launch vehicle.
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