GE-1A launch timeline
SPACEFLIGHT NOW
Posted: October 1, 2000
| 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+0:01:10 |
| Stage two ignition | T+0:02:00 |
| Stage one/two separation | T+0:02:06.7 |
| Stage two engine shut down | T+0:05:30.0 |
| Stage two/three separation | T+0:05:32.0 |
| Stage three main engine ignition | T+0:05:35.0 |
| Payload fairing jettison | T+0:05:37.0 |
| Stage three main engine shutdown | T+0:09:30 |
| Stage three/Block DM upper stage separation | T+0:09:48.7 |
| Block DM upper adapter jettison | T+0:10:43.7 |
| Block DM first burn ignition | T+1:13:49 |
| Block DM first burn shutdown | T+1:20:31 |
| Block DM second burn ignition | T+6:20:04 |
| Block DM/GE-1A payload separation | T+6:41:54 |
Data source: International Launch Services.
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Flight data file
Vehicle: Proton/Block DM
Payload: GE-1A
Launch date: Oct. 1, 2000
Launch window: 2200 GMT (6:00 p.m. EDT)
Launch site: LC 81, Pad 23, Baikonur Cosmodrome, Kazakhstan
Pre-launch briefing
Proton - Description of the Russian-made rocket used in this launch.
GE-1A - Learn more about the Proton's satellite cargo.
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