Michibiki 1

Launch Success

Liftoff Time (GMT)

11:17:00

Saturday September 11, 2010

Watch Replay

Official Livestream

Mission Details

Michibiki 1

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. 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. The QZS 1 is based on Mitsubishi's ETS-8-Bus and will have a lift off weight of 4100 kg. The QZS satellites are to operate for more than 10 years. Three more improved QZSS satellites have been ordered in April 2013. QZS-2 and QZS-4 will also operate from the inclined 24 hour orbit, while QZS-3 will augment the system from a geostationary orbit.

Geostationary Transfer Orbit

1 Payload

4,100 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


18th

Mission

2nd

Mission of 2010

2010


47th

Orbital launch attempt