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Michibiki (QZS-1) - Space launch mission detailed information

MISSION NAME

Michibiki (QZS-1) 1

Status

Success

DATE

11 SEP 2010

LAUNCH PROVIDER

Mitsubishi Heavy Industries + -img

Mitsubishi Heavy Industries

Launch Pad

Yoshinobu Launch Complex LP-1

JPN

Description

The Quasi-Zenith Satellite System (QZSS) is a three-satellite regional time transfer system and the satellite-based augmentation system for the GPS that would be receivable within Japan. The primary purpose of QZSS is to increase the availability of GPS in Japan's numerous urban canyons, where only satellites at very high elevation can be seen. A secondary function is performance enhancement, increasing the accuracy and reliability of GPS derived navigation solutions. A single satellite weighs about 4000 kg, has an expected lifetime of 15 years and is put in a elliptical, highly inclined geosynchronous orbit.

H-IIA 202

H-IIA 202

JPN

Rocket Description

H-IIA (H2A) is an active expendable launch system operated by Mitsubishi Heavy Industries (MHI) for the Japan Aerospace Exploration Agency. The liquid-fueled H-IIA rockets have been used to launch satellites into geostationary orbit, to launch a lunar orbiting spacecraft, and to launch Akatsuki, which studied the planet Venus. Launches occur at the Tanegashima Space Center.

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