Soyuz Flight Profile (Kanopus-V 3, 4 & Others)
Launch Timeline
| Time | Event |
|---|---|
| T-0:00:20 | Launch Command |
| T-0:00:14 | Preliminary Thrust Level |
| T-0:00:05 | To Full Thrust Level |
| T+0:00:00 | LIFTOFF |
| T+0:01:58 | Booster Separation |
| T+0:03:48 | Payload Fairing Jettison |
| T+0:04:46 | Core Stage Shutdown |
| T+0:04:47 | 3rd Stage Ignition & Staging |
| T+0:04:57 | Aft Section Cover Jettison |
| T+0:08:49 | 3rd Stage Separation |
| T+0:08:54 | Fregat First Burn |
| Burn Duration: 0:55 | |
| T+0:09:49 | Fregat Upper Stage Cutoff |
| T+0:55:42 | Fregat Re-Start |
| Duration: 01:25 | |
| T+0:57:17 | Fregat Shutdown |
| T+0:58:57 | Kanopus-V No.3 Separation |
| T+1:04:47 | Kanopus-V No.4 Separation |
| T+1:36:40 | Fregat Re-Start |
| Duration: 01:07 | |
| T+1:37:47 | Fregat Shutdown |
| T+2:19:10 | Fregat Re-Start |
| Duration: 01:06 | |
| T+2:20:16 | Fregat Shutdown |
| T+2:25:44 | S-NET Separation (10sec Intervals) |
| T+2:29:54 | Separation of 4 x Lemur-2 & D-Star ONE 1.1 |
| T+3:10:00 | Fregat Orbit-Lowering Sequence (2 Burns) |
| Duration: 1:01:40 | |
| T+4:51:10 | Fregat Deorbit Burn |
| Duration: 01:48 | |
| T+5:37:26 | Fregat Re-Entry (Pacific Ocean) |
Mission Data
Mission: Soyuz / Kanopus-V 3 & 4
Launch Vehicle: Soyuz 2-1A / Fregat
Launch Site: 1S Vostochny Cosmodrome
Primary Payload: Kanopus-v No.3 & 4 (2 x 490kg)
Secondary Payloads: 4 x S-NET, 4 x Lemur-2, D-Star ONE v.1.1 Phoenix
Launch Date: February 1, 2018
Launch Time: 02:07:18 UTC
Mission Duration: 5 Hours & 27 Minutes
Mission Design: Two-Orbit Mission w/ Deorbit
Orbital Data
Kanopus Target Orbit:
Type: Sun Synchronous Orbit
Perigee: 479 km
Apogee: 529 km
Inclination: 97.44°
Secondary Payload Target Orbit:
Type: Sun Synchronous Orbit
Perigee: 564 km
Apogee: 567 km
Inclination: 97.72°
Photo: Roscosmos
