Launch Profile – Minotaur-C

Launch Vehicle: Minotaur-C 3210

Launch Site: SLC-576E Vandenberg

Launch Date: October 31, 2017
Window: 21:37 UTC
Payload: 6 SkySat & 4 Flock-3m

Target Orbit:

Type: Sun Synchronous Orbit

Perigee: 500Kilometers
Apogee: 500 Kilometers

Equator Crossing: 13:30

Credit: Orbital ATK

Time	Event	Altitude (km)	Velocity (m/s)	Range (km)
T-0	Castor 120 Ignition (Stage 0)
T+01:25.5	Stage 0 Separation / Stage 1 Ignition	49.2	1,824	68
T+02:44.2	Stage 1 Burnout	144.7	4,267	320
T+02:49.3	Stage 1 Separation	150.5	4,254	320
T+02:51.5	Stage 2 Ignition	152.9	4,250	329
T+02:58.0	Payload Fairing Jettison	160.1	4,265	356
T+04:09.4	Stage 2 Burnout	242.0	6,667	745
T+05:13.4	Stage 2 Separation	313.4	6,568	1,165
T+09:16.0	Stage 3 Ignition	494.0	6,325	2,693
T+10:27.2	Stage 3 Burnout	507.0	7,609	3,163
T+13:22.2	SkySat #1 Separation
T+13:42.2	SkySat #2 Separation
T+14:02.2	SkySat #3 Separation
T+14:22.2	SkySat #4 Separation
T+15:22.2	Upper Bulkhead Separation
T+16:42.9	SkySat #5 Separation
T+17:02.9	SkySat #6 Separation
T+18:12.9	Flock-3m 1 & 2 Separation
T+19:44.4	Flock-3m 3 & 4 Separation
T+21:25.9	End of Mission