Mars Orbiter Mission
Mission profile

Mars Orbiter Mission

Section Title: Mission profile
Table Section Text: None

Phase	Date	Event	Detail	Result	References

Geocentric phase	5 November 2013 09:08 UTC	Launch	Burn time: 15:35 min in 5 stages	Apogee: 23,550 km (14,630 mi)

6 November 2013 19:47 UTC	Orbit raising manoeuvre	Burn time: 416 sec	Apogee: 28,825 km (17,911 mi)

7 November 2013 20:48 UTC	Orbit raising manoeuvre	Burn time: 570.6 sec	Apogee: 40,186 km (24,970 mi)

8 November 2013 20:40 UTC	Orbit raising manoeuvre	Burn time: 707 sec	Apogee: 71,636 km (44,513 mi)

10 November 2013 20:36 UTC	Orbit raising manoeuvre	Incomplete burn	Apogee: 78,276 km (48,638 mi)

11 November 2013 23:33 UTC	Orbit raising manoeuvre (supplementary)	Burn time: 303.8 sec	Apogee: 118,642 km (73,721 mi)

15 November 2013 19:57 UTC	Orbit raising manoeuvre	Burn time: 243.5 sec	Apogee: 192,874 km (119,846 mi)

30 November 2013, 19:19 UTC	Trans-Mars injection	Burn time: 1328.89 sec	Heliocentric insertion

Heliocentric phase	December 2013 – September 2014	En route to Mars – The probe travelled a distance of 780,000,000 kilometres (480,000,000 mi) in a Hohmann transfer orbit around the Sun to reach Mars.

11 December 2013 01:00 UTC	1st Trajectory correction	Burn time: 40.5 sec	Success

9 April 2014	2nd Trajectory correction (planned)	Not required	Rescheduled for 11 June 2014

11 June 2014 11:00 UTC	2nd Trajectory correction	Burn time: 16 sec	Success

August 2014	3rd Trajectory correction (planned)	Not required

22 September 2014	3rd Trajectory correction	Burn time: 4 sec	Success

Areocentric phase	24 September 2014	Mars orbit insertion	Burn time: 1388.67 sec	Success

Sentence(s)

The Apogee was raised to 28,825 km (17,911 mi).

final_sentence: The Apogee was raised to 28,825 km (17,911 mi).