Trajectory & orbital insertion
Ascent path is a representation — true ascent telemetry isn’t public.
Provider
Indian Space Research Organization
Provider type
Government
Orbit
—
Mission type
—
Launch site
India
Date
Sun, 02 Sep 2007 12:51:00 GMT
Orbital launch #
#4856 ever
Failure
Error in guidance subsystem caused low apogee and high inclination. Payload reached correct orbit on its own power.