Thanks! So it looks like the entire descent was telemetry-based (source [1], section 3.4):
The functions of the EDM GNC [Guidance, Navigation and Control system] are (1) to detect the
conditions adequate for the deployment of the
parachute and (2) to command and control the final
powered descent phase. The GNC sensors aboard the
EDM are the Inertial Measurement Unit (IMU) and the
Radar Doppler Altimeter (RDA). A main challenge for
the EDM GNC relates to the fact that the EDM needs
to go into a hibernation mode during the 3-day long
coast phase. During this phase, the inertial reference of
the IMU is lost and an additional sensor is necessary in
order to rebuild the inertial attitude shortly before
entry.