Flight Profile - Vega VV08
(Göktürk-1A)
Launch Timeline
Time | Event |
---|---|
T-0:04:00 | Start of Synchronized Sequence |
T-0 | P80 First Stage Ignition & Liftoff |
T+0:01:54 | P80 Separation |
T+0:01:55 | Zefiro-23 Second Stage Ignition |
T+0:03:37 | Zefiro-23 Separation |
T+0:03:54 | Zefiro-9 Third Stage Ignition |
T+0:03:59 | Payload Fairing Separation |
T+0:06:36 | Zefiro-9 Separation |
T+0:08:21 | AVUM - 1st Main Engine Start |
T+0:08:21 | Burn Duration: 6 Min & 19 Sec |
T+0:14:40 | AVUM - 1st Shutdown |
T+0:54:01 | AVUM - 2nd Main Engine Start |
T+0:54:01 | Burn Duration: 1 Min & 42 Sec |
T+0:55:43 | AVUM - 2nd Shutdown |
T+0:57:19 | Göktürk-1 Separation |
T+1:46:10 | AVUM - 3rd Main Engine Start (Deorbit) |
T+1:47:36 | AVUM - 3rd Shutdown |
T+2:00:56 | Vega - End of Mission |
Launch Info
Launch Vehicle: Vega
Launch Site: ZLV, French Guiana
Launch Date: December 5, 2016
Launch Time: 13:51:44 UTC
Payloads: Göktürk-1A (1,060kg)
Mission Duration: 2 Hours & 1 Minute
Target Orbit
Type: Sun Synchronous Orbit
Altitude: 700 Kilometers
Inclination: 98.11°