ASTRA 2C launch timeline
SPACEFLIGHT NOW
Posted: June 14, 2001
| Event | Time (h:mm:ss) |
| Stage one ignition | T-0:00:01.6 |
| Begin stage one thrust to 100% | T-0:00:00 |
| Liftoff | T+0:00:00.57 |
| Stage one thrust to 100% | T+0:00:01 |
| Maximum dynamic pressure | T+0:01:06 |
| Stage two ignition | T+0:02:00 |
| Stage one/two separation | T+0:02:06.7 |
| Stage two engine shut down | T+0:05:34.4 |
| Stage two/three separation | T+0:05:35.1 |
| Stage three main engine ignition | T+0:05:40.5 |
| Payload fairing jettison | T+0:05:44.2 |
| Stage three main engine shutdown | T+0:09:38 |
| Stage three/Block DM upper stage separation | T+0:09:54 |
| Block DM first burn ignition | T+1:13:45 |
| Block DM first burn shutdown | T+1:20:22 |
| Block DM second burn ignition | T+6:32:57 |
| Block DM second burn shutdown | T+6:34:56 |
| Block DM/PAS-10 payload separation | T+6:54:56 |
Data source: International Launch Services.
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Flight data file
Vehicle: Proton/Block DM
Payload: ASTRA 2C
Launch date: June 16, 2001
Launch time: 0149 GMT (9:49 p.m. EDT on June 15)
Launch site: LC 81, Pad 23, Baikonur Cosmodrome, Kazakhstan
Satellite broadcast: Telstar 5, Trans. 23, C-band
Pre-launch briefing
Proton - Description of the Russian-made rocket used in this launch.
ASTRA 2C - Learn more about the Proton's satellite cargo.
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