Minotaur IV - ORS-5 - Launch Profile

Launch Data
Launch Vehicle: Minotaur IV - Orion 38
Launch Site: SLC-26 Cape Canaveral
Launch Date: August 26, 2017
Window: 03:15-07:15 UTC
Payload: ORS-5 (140kg)
Satellites: SensorSat (113kg), 3 CubeSats
 
Backup Date: August 27, 2017

Target Orbit:
Type: Equatorial Low Earth Orbit
Perigee: 600 Kilometers
Apogee: 600 Kilometers
Inclination: 0.0 °
Photo: U.S. Air Force
Photo: U.S. Air Force
Launch Timeline

Time Event Altitude (km) Velocity (km/s) Range (km)
T+00:00 SR-118 Ignition & LIFTOFF 0.00 0.00 0.00
T+00:36 Maximum Dynamic Pressure 9.97 0.72 6.02
T+00:56.5 Stage 1 Sep / SR-119 Ignition 25.65 1.32 20.38
T+01:54 Stage 2 Burnout 92.65 3.86 141.67
T+02:05 Stage 2 Sep / SR-120 Ignition 105.46 3.84 177.49
T+02:24 Payload Fairing Separation 130.10 4.35 252.38
T+03:17.5 Stage 3 Burnout 194.00 6.88 529.20
T+13:44.5 Stage 3 Separation 571.49 6.38 4369.15
T+13:55 Orion-38 (Stage 4) Ignition 572.77 6.38 4433.55
T+15:02 Stage 4 Burnout 578.01 7.07 4840.23
T+17:02 CubeSat #1 Separation
T+17:32 CubeSat #2 Separation
T+18:02 CubeSat #3 Separation
T+25:08 Stage 4 Separation 598.83 7.05 8746.92
T+25:18.5 Orion-38 (Stage 5) Ignition 598.82 7.05 8817.70
T+26:27.5 Stage 5 Burnout 600.70 7.05 9256.20
T+28:27.5 Sensor Sat Separation 600.78 7.05 9935.89
T+33:27.5 Reaction Control System Blowdown 600.30 7.05 11622.42
T+36:48 End of Mission 599.53 7.05 12728.85

Image: Orbital ATK
Image: Orbital ATK