H-IIA 204 | Michibiki 3 (QZS-3)

H-IIA 204 | Michibiki 3 (QZS-3) rode a H-IIA into space from Tanegashima Space Center, Japan, deploying its payload to GTO.

Launch time
Status
SUCCESS
Operator
Mitsubishi Heavy Industries
Mission type
Navigation
Rocket
H-IIA
Launch pad
Yoshinobu Launch Complex LP-1
Payload
—
Target orbit
GTO
H-IIA 204 | Michibiki 3 (QZS-3) cover image

Mission timeline

  1. 2017-08-19T05:29:00.000Z
    Liftoff
    Liftoff confirmed — H-IIA is airborne.
  2. Max-Q
    Max Q — H-IIA endures peak structural stress during ascent.
  3. Main engine cutoff (MECO)
    First-stage main engine cutoff (MECO) confirmed.
  4. Stage separation
    The spent first stage separates from the upper stage.
  5. Second-stage ignition
    Upper stage ignites, continuing the journey toward orbit.
  6. Orbit insertion
    The mission reaches GTO, successfully entering orbit.
  7. Mission success
    The mission concludes successfully.

Last updated: