June 1, 2017 12:17 am

Michibiki 2 (QZS-2)

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H-IIA

Tanegashima Space Center, Japan
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June 1, 2017 12:17 am

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2026-07-11 21:41:11

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.
Launch Overview
Window Open 00:17 UTC
Window Close 00:17 UTC
Lift Off Jun 1, 2017 · 00:17 UTC
Launch Facility Tanegashima Space Center, Japan
Launch Pad Yoshinobu Launch Complex LP-1
Target Orbit Geosynchronous Transfer Orbit
Payload Overview
Customer Mitsubishi Heavy Industries
Payload Michibiki 2 (QZS-2)
Rocket H-IIA
Destination Geosynchronous Transfer Orbit
Recovery Overview
Landing Location See Mission Notes
Landing Type RTLS / Droneship
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.

Height

LEO Payload

Total Launches

Status

Mitsubishi Heavy Industries
Yoshinobu Launch Complex LP-1
Launch Overview
Window Open 00:17 UTC
Window Close 00:17 UTC
Lift Off Jun 1, 2017 · 00:17 UTC
Launch Facility Tanegashima Space Center, Japan
Launch Pad Yoshinobu Launch Complex LP-1
Target Orbit Geosynchronous Transfer Orbit
Payload Overview
Customer Mitsubishi Heavy Industries
Payload Michibiki 2 (QZS-2)
Rocket H-IIA
Destination Geosynchronous Transfer Orbit
Recovery Overview
Landing Location See Mission Notes
Landing Type RTLS / Droneship

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