Launch and docking Progress M1-5 was launched by a
Soyuz-U carrier rocket from the
Baikonur Cosmodrome,
Kazakhstan. It was originally scheduled for launch on 16 January 2001, but by the first week of January, it was targeting 18 January. Launch was set for 06:56:26 GMT on 18 January. On the day, a problem with the computers aboard
Mir developed shortly before fuelling of the Soyuz-U rocket was scheduled to commence, about five and a half hours before the launch was due to occur. The launch attempt was
scrubbed, or cancelled, and the launch was expected to be delayed by four or five days. On 19 January, the launch was rescheduled for 24 January, giving controllers time to restart the computer and the station's
gyroscopes, which had shut down when the computer failed. Preparations for the launch resumed on 22 January, and the launch occurred successfully at 04:28:42 GMT on 24 January. Following the launch, Progress M1-5 spent three days in free flight before docking with the rear port of the
Kvant-1 module of
Mir at 05:33:31 GMT on 27 January. The docking port had previously been occupied by
Progress M-43, which departed at 05:19:49 on 25 January, Progress M-43, which had originally been launched to carry supplies and raise
Mir's orbit, in anticipation of crewed flights which were never launched, was subsequently deorbited at 02:12 GMT on 29 January, burning up during re-entry at 02:58. Following the docking,
Mir's
attitude control system was used to spin the station, to provide
spin-stabilisation in order to further conserve the fuel, as the station had descended to an altitude at which its gyroscopes could not be used for attitude control. The station would remain in this spin until the deorbit manoeuvres began. On 20 February,
Mir was predicted to descend to 250 kilometres within five days of 9 March. along with the control system on 13 March. On 14 March it was announced that the procedure would be conducted on 22 March. On 19 March it was delayed one day further due to a lower than expected descent rate, with the start of the first deorbit burn being set for 00:31 GMT.
Deorbit Progress M1-5 carried of fuel with which to perform the manoeuvres to deorbit
Mir. These were completed on 23 March, when three deorbit burns were made; the first two using just docking and attitude control thrusters, and the third using the main engine as well as the thrusters. The first burn began at 00:32:28 GMT, and lasted 21.5 minutes, leaving
Mir in an orbit with a
perigee of and an
apogee of . It was scheduled to last 20 minutes, however flight controllers decided to let the Progress burn to depletion to ensure that the station re-entered as expected.
Mir re-entered the atmosphere over the southern Pacific with Progress M1-5 still docked at 05:44 GMT. It began to disintegrate at 05:52, beginning with the detachment of solar panels, followed by other peripheral structures. The modules then buckled, before detaching completely. Debris was intended to fall at around . An official statement announced that
Mir "ceased to exist" at 05:59:24 GMT. The
European Space Agency, German
Federal Ministry of Defence and US
National Aeronautics and Space Administration also assisted with tracking
Mir during its final orbit and reentry. Former
cosmonaut Vladimir Solovyov, who had been a member of the first crew to visit
Mir, led the mission control team which was on station during the deorbit. == Contingency planning ==