Chandrayaan-2 will launch on a GSLV Mark-III from Satish Dhawan Space Centre. It consists of three parts, with a total mass at launch of about 2,400 kg:

• Orbiter
• Vikram Lander
• Pragyan Rover

After launch, from here:

...the cryogenic upper stage, powered by CE-20, India's largest cryogenic engine, will ignite, driving the module to a highly elliptical Earth Parking Orbit.

At this stage, the onboard propulsion system will raise the module’s orbit around the Earth through a number of burn. How does this work, you may ask?

[...] The closer the module is to the Earth, the more the gravitational pull, and the greater the speed. Every time the module reaches the perigee, or the point of highest speed, the onboard engine fires, increasing its speed even more, pushing it into a higher, more elongated orbit as a result. With every burn of the onboard propulsion system, the module will keep spiralling outwards in increasingly elongated ellipses.

It's not really a spiral, the perigee remains fairly constant.

Burning only at perigee where velocity is maximum is taking advantage of the Oberth effect, something you can read about in the several excellent answers to Oberth effect for Earth vehicles, or here.

I don't know the details of the burns yet. This article India set to launch second moon mission Chandrayaan-2 in July, landing by September says:

Orbital path

Just like Chandrayaan-1 and Mars Orbiter Mission, the Chandrayaan-2 will also perform orbit raising manoeuvres around the Earth six times to gain the required height and speed to break away from the Earth’s gravity.

This six-step process is a staple procedure followed by the ISRO with the objective of reducing cost of fuel and launching with a home-grown rocket that is as of now incapable of flying directly to the moon, like Saturn V rocket did for the Apollo missions.

However, here is a table of Chandrayaan-1's burns from here:

Date (UTC)    Burn time (min)    Resulting apogee (km)
22 October        Launch            22,860
23 October          18              37,900 
25 October          16              74,715
26 October          9.5            164,600
29 October          3              267,000
 4 November         2.5            380,000

There will likely be a check of the trajectory after each burn, and there are several adjustments that need to be made before the Lunar Transfer Trajectory (LTT) can be reached.

Satish Dhawan Space Centre is close to 14 N latitude, which means it can potentially launch into a 24° inclination orbit to match the Moon's inclination with respect to Earth's equator. However, the delicate LTT maneuver will have a small window in time and position so that the spacecraft can be in just the right place, at just the right time to be captured into lunar orbit without using a huge amount of valuable propellant.

Hitting this "keyhole" in both space and time will be difficult, and so Chandrayaan-2 will take its time, step by step in order to be captured into lunar orbit with a minimum amount of propellant usage.

All eyes will be on ISRO and Chandrayaan-2 for several reasons.

1. ISRO is hot! They have had an excellent run in deep-space missions to the Moon and to Mars, and this moon orbiter, lander, and rover are a new thing for this space agency.
2. This is the 50th anniversary of the Apollo-11 Moon landing, and so there is a lot of extra moon hype going around.