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GSLV-3
Part of GSLV
The Indian Geosynchronous Satellite Launch Vehicle Mark III was developed by ISRO to launch satellites into geostationary orbit and as a launcher for an Indian crew vehicle. The GSLV-3 featured an Indian cryogenic third stage and a higher payload capacity than the earlier GSLV models.
 Status: Active.  First Launch: 2014-12-18.  Last Launch: 2018-11-14.  Number:  3 . 
Country: 
India. 
Spacecraft: 
Indian Manned Spacecraft. 
Launch Sites: 
Sriharikota SLP. 
2014 December 18 - . 
04:00 GMT - . 
Launch Site: 
Sriharikota. 
Launch Complex: 
Sriharikota SLP. 
 
Launch Pad: Srikarikota SLP. 
LV Family: 
GSLV. 
Launch Vehicle: 
GSLV-3. 
- CARE/LVM3-X - . 
Mass: 3,735 kg (8,234 lb). Nation: India. 
Class: Manned. 
 Type: Manned spacecraft. Spacecraft: Indian Manned Spacecraft. 
Apogee: 126 km (78 mi). Launch of the first GSLV-III rocket on a suborbital test flight. The S200 solid boosters and L110 core stage, with two Vikas engines, propelled an inert second stage to 126 km and 5.3 km/s. Second stage separation and payload separation were also tested; the payload was the
Crew Module Atmospheric Reentry Experiment, a prototype command module
for an Indian manned spacecraft with a mass of 3735 kg which splashed down in the Bay of Bengal. Orbit was around -4418 x 126 km x 32.7 deg. 
2017 June 5 - . 
11:57 GMT - . 
Launch Site: 
Sriharikota. 
Launch Complex: 
Sriharikota SLP. 
LV Family: 
GSLV. 
Launch Vehicle: 
GSLV-3. 
- GSAT-19E - . 
Nation: India. 
 USAF Sat Cat:  42747 .  COSPAR: 2017-031A. Apogee: 35,805 km (22,248 mi). Perigee: 35,766 km (22,223 mi). Inclination: 0.0700 deg. Period: 1,436.05 min. See GSat 19. .. 
2018 November 14 - . 
11:37 GMT - . 
Launch Site: 
Sriharikota. 
Launch Complex: 
Sriharikota Dhawan SLP. 
LV Family: 
GSLV. 
Launch Vehicle: 
GSLV-3. 
- GSAT-29 - . 
Nation: India. 
 Type: Comms.  USAF Sat Cat:  43698 .  COSPAR: 2018-089A. Apogee: 35,797 km (22,243 mi). Perigee: 35,776 km (22,230 mi). Inclination: 0.00 deg. Period: 1,436.08 min. See GSat 29. .. 
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