The apogee raise maneuver of IRNSS-1F has been successfully carried out for 1192 sec from 16:16 hrs IST on March 11, 2016.

Orbit Determination results from this LAM firing are:

apogee X perigee height was changed to 35828 kmX 318.5 km. Inclination is 17.86 deg. Orbital period is 10hr 34min.