About the final phase of OC Mir flight.
23 March 2001 (Moscow time)

03.32 AM  - the first impulse is performed using the Progress M1-5 eight thrusters to construct the  pre-descent orbit.

Value of impulse - 9,3 m/s

The orbit parameters after maneuver :

-          maximal distance from earth surface - 219 km

-          minimal distance from earth surface - 188 km

-          period of revolution - 88,4 min

05.00.24 AM  - the second impulse is performed using the Progress M1-5 eight thrusters to construct the  pre- descent orbit.

  Value of impulse - 10,4 m/s

The orbit parameters after maneuver :

-          maximal distance from earth surface - 219 km

-          minimal distance from earth surface - 158 km

-          period of revolution - 88,1 min

08.08 AM  - the final third breaking impulse is performed using a combination of the Progress M1-5 main engine and eight thrusters to deorbit Mir OC.

Value of impulse was 28 m/s

The ellipse dissipation centre coordinates of unburned fragments: 40^o south latitude; 160,0^o west longitude