Michibiki 4

Launch Success

Liftoff Time (GMT)

22:01:37

Monday October 9, 2017

Watch Replay

Official Livestream

Mission Details

Michibiki 4

Wiki

QZSS (Quasi Zenith Satellite System) is a Japanese satellite navigation system operating from inclined, elliptical geosynchronous orbits to achieve optimal high-elevation visibility in urban canyons and mountainous areas, as well as from geostationary orbits. The navigation system objective is to broadcast GPS-interoperable and augmentation signals as well as original Japanese (QZSS) signals from a three-spacecraft constellation. Phase one will demonstrate the technological validation for the enhancement of GPS availability and performance and their application, using the first Quasi-Zenith Satellite (QZS 1) Michibiki. After evaluating these results, the plan moves into phase two which demonstrates the full system capability using three Quasi-Zenith Satellites, including QZS-1. JAXA is in charge of integrating the system as a whole, as well as cooperating with related research organizations to develop the High Accuracy Positioning Experiment System, the QZS Bus System and the Tracking Control System.

Geostationary Transfer Orbit

1 Payload

4,000 kilograms

Rocket

Retired
H-IIA 202

Active 2001 to 2025

Mitsubishi Heavy Industries logo

Agency

MHI

Price

$90.00 million

Rocket

Height: 53m

Payload to Orbit

LEO: 10,000 kg

GTO: 4,100 kg

Fairing

Diameter: 4.07m

Height: 12m

Stages

2

Strap-ons

2

Launch Site

LA-Y1

Tanegashima Space Center, Japan

Fastest Turnaround

25 days 4 hours

Stats

H-IIA


36th

Mission

5th

Mission of 2017

2017


66th

Orbital launch attempt