Here's a Google Translation of the Mission Events. Fregat SB to perform three burns after being directly inserted into a roughly 167 x 554 km x 51.35 deg parking orbit by Zenit. The first burn will put the vehicle into a 280 x 4,306 km x 50.4 deg intermediate orbit. Drop tanks will jettison shortly after the burn. The second burn will push the vehicle into a 338 x 35,911 km x 48.6 deg geosynchronous transfer orbit. The third burn will boost the vehicle into near GEO.
UTC
Mission Elapsed Time
Event
13:45:33
0:00:00
Start RN
13:47:58
0:02:25
Separation of the 1st and 2nd stages RN
13:50:50
0:05:17
Issuing commands to secede fairing
13:54:07
0:08:34
Issue the command to shut down the propulsion system (PS), the second stage of the launch
13:54:08
0:08:35
Department head unit from the second stage of
14:59:12
1:13:39
Turning control stabilization, orientation and provide start-up RB
15:00:07
1:14:34
1st march switch control RB
15:08:32
1:22:59
Switching off the cruise control Belarus
15:09:09
1:23:36
Issuing commands to the Department discharged tanks block RB
15:09:09
1:23:36
Output head unit to an intermediate orbit
17:10:55
3:25:22
Second switch control stabilization, orientation and ensure proper ignition
17:11:50
3:26:17
Second switch control Marching RB
17:22:48
3:37:15
Switching off the cruise control Belarus
17:22:58
3:37:25
Out headunit to geosynchronous transfer orbit
22:31:13
8:45:40
Third switch control stabilization, orientation and provide start-up RB
22:32:08
8:46:35
3rd march inclusion of control RB
22:40:56
8:55:23
Switching off the cruise control Belarus
22:43:26
8:57:53
Issuing commands to separate the spacecraft "Electro-L» № 2
- Ed Kyle