H-IIA F34 Flight Profile (QZS-2)

Launch Vehicle: H-IIA 202
Launch Site: Tanegashima Space Center
Launch Date: June 1, 2017
Launch Time: 0:17:46 UTC
Payload: Quasi-Zenith Satellite 2 (4,100kg)
Ascent Duration: 28 Min & 24 Sec

Target Orbit:
Type: Tundra Transfer Orbit
Perigee: 250 Kilometers
Apogee: 36,140 Kilometers
Inclination: 31.9 Degrees
 
Operational Orbit:
Type: Tundra Orbit
Semi-Major Axis: 42,164 km
Eccentricity: 0.075
Inclination: 44°
Period: 23 Hours 56 Minutes
Image: JAXA
Image: JAXA
Ascent Timeline

Time Event Altitude (km) Velocity (km/s)
T-00.05 LE-7A Ignition 0 0.4
T-00:00 SRB-A3 Ignition & LIFTOFF 0 0.4
T+01:38 SRB-A3 Burnout 46 1.5
T+01:48 SRB-A3 Separation 54 1.5
T+04:10 Payload Fairing Separation 151 2.6
T+06:38 MECO - LE-7A Shutdown 234 5.2
T+06:46 Stage Separation 239 5.2
T+06:52 LE-5B Ignition 242 5.2
T+12:34 Second Stage - 1st Shutdown 292 7.7
T+24:34 LE-5B Re-Ignition 256 7.7
T+27:34 Second Stage - 2nd Shutdown 254 10.2
T+27:57 QZS-2 Separation 274 10.2

Ground Track Map
Image: JAXA/Spaceflight101
Image: JAXA/Spaceflight101