H-IIA F36 Flight Profile (QZS-4)
Launch Vehicle: H-IIA 202
Launch Site: Tanegashima Space Center
Launch Date: October 9, 2017
Launch Time: 22:01:37 UTC
Payload: Quasi-Zenith Satellite 4 (4,000kg)
Launch Time: 22:01:37 UTC
Payload: Quasi-Zenith Satellite 4 (4,000kg)
Ascent Duration: 28 Min & 24 Sec
Target Orbit:
Type: Tundra Transfer Orbit
Perigee: 250 Kilometers
Apogee: 36,140 Kilometers
Inclination: 31.9 Degrees
Apogee: 36,140 Kilometers
Inclination: 31.9 Degrees
Operational Orbit:
Type: Tundra Orbit
Semi-Major Axis: 42,164 km
Eccentricity: 0.075
Inclination: 41°
Period: 23 Hours 56 Minutes
Ascent Timeline
Time | Event | Altitude (km) | Velocity (km/s) | Range (km) |
---|---|---|---|---|
T-00.05 | LE-7A Ignition | 0 | 0.4 | 0 |
T-00:00 | SRB-A3 Ignition & LIFTOFF | 0 | 0.4 | 0 |
T+01:38 | SRB-A3 Burnout | 46 | 1.5 | 31 |
T+01:48 | SRB-A3 Separation | 54 | 1.5 | 38 |
T+04:10 | Payload Fairing Separation | 151 | 2.6 | 238 |
T+06:38 | MECO - LE-7A Shutdown | 234 | 5.2 | 705 |
T+06:46 | Stage Separation | 239 | 5.2 | 742 |
T+06:52 | LE-5B Ignition | 242 | 5.2 | 770 |
T+12:34 | Second Stage - 1st Shutdown | 292 | 7.7 | 2,690 |
T+24:34 | LE-5B Re-Ignition | 256 | 7.7 | 7,725 |
T+27:34 | Second Stage - 2nd Shutdown | 254 | 10.2 | 9,180 |
T+28:24 | QZS-4 Separation | 274 | 10.2 | 9,652 |