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The Japanese H-2A rocket will launch the Michibiki navigation satellite. Also called the Quasi-Zenith Satellite, Michibiki will enhance GPS navigation signals in Japanese urban areas and mountainous terrain. The H-2A rocket will fly in the 202 configuration with two large solid rocket boosters and no smaller motors.

Launch window:|11:17-12:16 UTC / 7:17-8:16 a.m. EDT / 20:17-21:16 JST
Launch site:|Tanegashima Space Center, Japan
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There is O-F's calendar event created for this launch, for which you can request a reminder, that will be sent via e-mail on set time before the launch.
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Payload:
Launch Vehicle:
Live coverage of the launch:
Links:
JAXA Press Releases:
Launch Sequence:
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Event
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Time [mm:ss]
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Altitude [km]
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Inertial speed [km/s]
*) When the maximum combustion pressure reaches 2%
**) Thrust strut cutoff
Launch site:|Tanegashima Space Center, Japan
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[highlight]L[eventtimer]2010-9-11 11:17;%c%%ddd%/%hh%:%mm%:%ss%[/eventtimer][/highlight]
There is O-F's calendar event created for this launch, for which you can request a reminder, that will be sent via e-mail on set time before the launch.
Mission Logo
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Mascot Character - "MICHIBIKI-San"
Payload:
The Quasi-Zenith Satellite System (QZSS) is a regional space-based positioning system that uses a constellation of satellites placed in multiple orbital planes. The satellites have the same orbital period as a traditional equatorial geostationary orbit, however, they have a large orbital inclination and therefore move with respect to the Earth. The QZS orbits are also elliptical and are sometimes known as “highly-inclined elliptical orbits” or HEO. The system covers regions in East Asia and Oceania centering on Japan and is designed to enable users in the coverage area to receive QZS signals from a high elevation angle at all times.
The nickname “MICHIBIKI,” meaning "guiding" or "showing the way,” was selected as a nickname for the first Quasi-Zenith Satellite (QZS-1) through a campaign conducted between October 16 (Fri.) and December 16 (Wed.), 2009, where 328 people out of 11,111 participants proposed “MICHIBIKI” as a nickname. Many godparents of "MICHIBIKI" explained their selection reason as the QZS-1 is to show correct locations using its highly accurate positioning information, and to guide toward a futuristic society by establishing the next generation satellite positioning technology in Japan. The name was chosen as it precisely illustrates the QZS mission.
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The nickname “MICHIBIKI,” meaning "guiding" or "showing the way,” was selected as a nickname for the first Quasi-Zenith Satellite (QZS-1) through a campaign conducted between October 16 (Fri.) and December 16 (Wed.), 2009, where 328 people out of 11,111 participants proposed “MICHIBIKI” as a nickname. Many godparents of "MICHIBIKI" explained their selection reason as the QZS-1 is to show correct locations using its highly accurate positioning information, and to guide toward a futuristic society by establishing the next generation satellite positioning technology in Japan. The name was chosen as it precisely illustrates the QZS mission.
Shape:
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- 2 box shape with wing-type solar array paddles
- 2.9m in depth x 3.1m in width x 6.2m in height
- Length between the tips of the paddles: 25.3 m
Mass:
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- Approx. 4000kg
Power:
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- About 5 kW
Lifetime:
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- Over 10 years
Orbit:
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- Quasi-Zenith Orbit
Altitude:
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- Apogee: approx. 32,000 km,
- Perigee: approx. 40,000 km
Inclination:
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- Approx. 40 degrees (Fluctuating between 39 and 47 degrees; 41 degrees in the initial phase.)
Period:
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- 23 hours 56 minutes
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QZSS constellation
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Trajectory footprint
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Tracking stations
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Launch Vehicle:
The H-IIA Launch Vehicle No. 18 is a "H2A202" model with two solid rocket boosters (SRBs). The fairing design is 4S (4 meters in diameter.) Mitsubishi Heavy Industries, Ltd. is in charge of the launch service of the H-IIA.
The mission of the H-IIA Launch Vehicle No. 18 is to inject its main payload, the Quasi-Zenith Satellite-1 "MICHIBIKI", into its scheduled orbit.
The mission of the H-IIA Launch Vehicle No. 18 is to inject its main payload, the Quasi-Zenith Satellite-1 "MICHIBIKI", into its scheduled orbit.
Live coverage of the launch:
- You can watch the webcast of the launch of H-2A F18 carring MICHIBIKI live here.
Live Broadcast of the launch is scheduled to start on Sept. 11, Saturday at 6:45 a.m. EDT / 10:45 UTC / 7:45 p.m. JST - i.e. it [eventtimer]2010-9-11 10:45?will start in|started;%c% %h%:%mm%[/eventtimer] hours[eventtimer]2010-9-11 10:45?.| ago.;%c%[/eventtimer] - Countdown Report - Final countdown status of H-IIA Flight F18 carrying MICHIBIKI will be reported there.
Links:
- MICHIBIKI Special Site.
- What is Quasi-Zenith Orbit?
- Overview of the First Quasi-Zenith Satellite "MICHIBIKI".
- Interview with Koji Terada, Establishment of a Seamless Positioning System.
- Positioning to know your location and time.
- Let's ask MICHIBIKI-san! Quasi-Zenith Satellite (QZS) 'MICHIBIKI' FAQ.
- Quasi-Zenith Satellite-1 "MICHIBIKI" Photo Gallery.
- Quasi-Zenith Satellite-1 "MICHIBIKI" Video Gallery.
- MICHIBIKI Wallpapers & Paper crafts.
MICHIBIKI Overview Brochure (PDF).
MICHIBIKI Press Kit (PDF).
Interface Specifications for QZSS (IS-QZSS Ver.1.1) (PDF).
Interface Specifications for QZSS (IS-QZSS Ver.1.2 Draft) with Revision Mark (PDF).
JAXA Press Releases:
- 2010-01-20: "MICHIBIKI" Chosen as Nickname of the first Quasi-Zenith Satellite.
- 2010-06-09: Launch (date announcement) of the First Quasi-Zenith Satellite 'MICHIBIKI' by the H-IIA Launch Vehicle No. 18.
- 2010-06-23: Launch Postponement of the First Quasi-Zenith Satellite 'MICHIBIKI' by H-IIA Launch Vehicle No. 18.
- 2010-08-04: New Launch Day of the First Quasi-Zenith Satellite 'MICHIBIKI' by H-IIA Launch Vehicle No. 18.
Launch Sequence:
1.
|Liftoff|
0:00
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0
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0.4
2.
|Solid rocket booster burnout*|
1:37
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45
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1.4
3.
|Solid rocket booster jettison**|
1:47
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54
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1.5
4.
|Payload fairing jettison|
4:10
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150
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2.6
5.
|1st stage engine (main engine) cutoff (MECO)|
6:36
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228
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5.2
6.
|1st and 2nd stages separation|
6:44
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223
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5.2
7.
|2nd stage 1st ignition (SEIG1)|
6:50
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236
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5.2
8.
|2nd stage engine 1st cutoff (SECO1)|
12:32
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288
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7.7
9.
|2nd stage 2nd ignition (SEIG2)|
24:34
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256
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7.7
10.
|2nd stage engine 2nd cutoff (SECO2)|
27:35
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254
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10.2
11.
|MICHIBIKI separation|
28:26
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275
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10.2
*) When the maximum combustion pressure reaches 2%
**) Thrust strut cutoff
The current view on Tanegashima Space Center (webcam). *
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* This picture is automatically updated at intervals.
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