SoyuzFlight Profile (73 Satellites)
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+0:04:45 | Core Stage Shutdown |
| T+0:04:47 | 3rd Stage Ignition & Staging |
| T+0:04:49 | Payload Fairing Jettison |
| T+0:04:57 | Aft Section Cover Jettison |
| T+0:08:48 | 3rd Stage Separation |
| T+0:08:53 | Fregat First Burn |
| Burn Duration: 6:36 | |
| T+0:15:29 | Fregat Upper Stage Cutoff |
| T+0:58:12 | Fregat Re-Start |
| Duration: 01:26 | |
| T+0:59:41 | Fregat Shutdown |
| T+1:01:18 | Kanopus V-IK Separation |
| T+1:36:40 | Fregat Re-Start |
| Duration: 01:06 | |
| T+1:37:46 | Fregat Shutdown |
| T+2:21:40 | Fregat Re-Start |
| Duration: 01:06 | |
| T+2:22:47 | Fregat Shutdown |
| T+2:24:54 | Separation of MicroSats (200 Seconds) |
| T+2:33:14 | Separation of 19 CubeSats (1,000 Seconds) |
| T+3:15:00 | Fregat Re-Start |
| Duration: 01:26 | |
| T+3:16:26 | Fregat Shutdown |
| T+3:57:50 | Fregat Re-Start |
| Duration: 01:12 | |
| T+3:59:01 | Fregat Shutdown |
| T+7:41:34 | Separation of Flock-2k (1,374 Seconds) |
| T+8:15:00 | Fregat Deorbit Burn |
| Duration: 01:56 | |
| T+8:42:00 | Fregat Re-Entry (Indian Ocean) |
Mission Data
Mission: Soyuz / Kanopus V-IK
Launch Vehicle: Soyuz 2-1A / Fregat-M
Launch Site: 31/6 Baikonur Cosmodrome
Primary Payload: Kanopus V-IK (600kg)
Secondary Payloads: 5 MicroSats (18-120kg), 67 CubeSats
Launch Date: July 14, 2017
Launch Time: 06:36:49 UTC
Mission Duration: 8 Hours & 42 Minutes
Mission Design: Three-Orbit Mission w/ Deorbit
Orbital Data
Kanopus V-IK Target Orbit:
Type: Sun Synchronous Orbit
Perigee: 478.6 km
Apogee: 522.5 km
Inclination: 97.44°
MicroSat Target Orbit:
Type: Sun Synchronous Orbit
Perigee: 590.1-600.0 km
Apogee: 600.1-601.5 km
Inclination: 97.61°
Satellites: Flying Laptop, WNISAT-1R, NORSat-1 & 2, TechnoSat
CubeSat Target Orbit:
Type: Sun Synchronous Orbit
Perigee: 580.1-587.4 km
Apogee: 601.0-606.9 km
Inclination: 97.61-97.62°
Satellites: CICERO-1, 2, 3, Corvus-BC 1 & 2, MKA-N 1 & 2, Mayak, NanoAce, Eight Lemur-2, Iskra-MAI-85, Ecuador-UTE-YuZGU
CubeSat Target Orbit:
Type: Sun Synchronous Orbit
Perigee: 450.5-482.2 km
Apogee: 477.4-485.0 km
Inclination: 97.00-97.01°
Satellites: 48 Doves (Flock-2k)
