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Launch status: GOMHI

H3-24 | Martian Moons eXploration (MMX)

Mitsubishi Heavy Industries launches H3-24 carrying Martian Moons eXploration (MMX) from Yoshinobu Launch Complex LP-2, Tanegashima Space Center, Japan at 2026-10-19 19:41:03Z. That T-0 is confirmed to the second. The vehicle is go for launch.

COUNTDOWN

GO
TIME TO T-0
T-··:··:··
ADD TO CALENDAR
NET (UTC)2026-10-19 19:41:03Z
WINDOWINSTANTANEOUS

FLIGHT PLAN

FILED
OPERATORMitsubishi Heavy Industries
VEHICLEH3-24
PAYLOADMartian Moons eXploration (MMX)
MISSION TYPEPlanetary Science
TARGET ORBITMars
VEHICLE FAMILYH3
PADYoshinobu Launch Complex LP-2
SITETanegashima Space Center, Japan
WINDOW OPEN2026-10-19 19:41:03Z
WINDOW CLOSE2026-10-19 19:41:03Z
NET PRECISIONSEC
REUSABLENO

The window is instantaneous: the vehicle flies at T-0 or stands down to the next opportunity. Current T-0 confirmed by official or reliable sources.

FIELD KIT / OPTICS

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MISSION BRIEF

FILED

MMX is a Japanese scientific mission to land on Phobos, one of the two moons of Mars, to collect samples before bringing them back to Earth. The mission includes a small French/German rover to explore the surface of Phobos.

SOURCE: LAUNCH LIBRARY 2 // THE SPACE DEVS

LAUNCH CORRIDOR

FROM THIS PAD
Due east
The lowest orbit inclination a direct launch from here can reach — 30.4°, which is this pad’s own latitude. It also collects the most free speed from Earth’s rotation.
Due south
The polar and sun-synchronous corridor: 90° inclination, passing over both poles. It gets no help from Earth’s spin, which is why it costs more payload.

Drag the globe to turn it. The shading is the real terminator, and it moves.

A globe of the Earth centred on Yoshinobu Launch Complex LP-2 at latitude 30.40 degrees north, longitude 130.98 degrees east. Two curved lines leave the pad. The solid gold line runs due east and marks the lowest orbital inclination a direct launch from this site can reach, 30.4 degrees, equal to the pad’s latitude of 30.4 degrees. The dashed cyan line runs due south and marks the polar corridor at 90 degrees inclination. The darkened part of the globe is the night side. Surface wind is blowing from 89°, at 19 km/h, shown as the cyan arrow at the pad.

LAUNCH SITE

FIXED
PAD DESIGNATION

Yoshinobu Launch Complex LP-2

Tanegashima Space Center, Japan

LATITUDE30°24′03″ N30.4009°
LONGITUDE130°58′32″ E130.9756°
90°N90°SEQUATORWIND FROM E · 19 km/h
180°W0° MERIDIAN180°E
PAD±30° BANDWIND (DOWNWIND)
ON SITE NOWWIND FROM E · 19 km/hCLEAR SKY25.8 °CCLOUD 16%

OBSERVED 2026-10-11 20:00:00Z // OPEN-METEO (CC BY 4.0) // GENERAL CONDITIONS, NOT LAUNCH CRITERIA

Minimum direct inclination 30°. From 30° north of the equator, a direct ascent cannot enter an orbit inclined less than 30°, because an orbit of inclination i never passes over latitudes beyond ±i. Reaching an equatorial plane — what a geostationary transfer ultimately needs — therefore costs a plane change of 30° somewhere in the flight, while inclinations of 30° and above are available straight off the pad. The ground here is carried eastward at about 401 m/s (465 m/s at the equator, falling with the cosine of latitude), and a due-east launch keeps that head start.

DATUM WGS-84 // EQUIRECTANGULAR PROJECTION // ORBIT FIGURES DERIVED FROM THE PUBLISHED LATITUDE

Site map of Yoshinobu Launch Complex LP-2, function n(a,b){let c=l(a)?a.trim():"",d=l(b)?b.trim():"";return c?d?(c.split(",").pop()?.trim().toLowerCase()??"")===d.toLowerCase()?c:`${c}, ${d}`:c:d}.
SITE PLAN // SOURCE: LAUNCH LIBRARY 2

PAD CONDITIONS

OBSERVED

SURFACE WIND @ 10 M

19km/h

Blowing from the east, bearing 89 degrees

GUSTING

21km/h

Clear sky

CLOUD COVER16%
WIND DIRE · 89°
PRECIP NOW0.0 mm
PRECIP CHANCE0%
TEMP25.8 °C
HUMIDITY66%
OBSERVED2026-10-11 20:00:00Z
STATION FIX30.401°, 130.976°

SOURCE: OPEN-METEO CC BY 4.0

The observed block is general weather for the coordinates of Yoshinobu Launch Complex LP-2, not launch-commit criteria. Those are written per mission by the operator and the range, cover conditions this forecast does not carry at all (electric fields, cloud layers aloft, winds through the vehicle’s own load limits), and are published only by the operator. Wind is a common reason countdowns stop for weather — that is general context, not a rule about this flight, and no number in this block is a threshold. Nothing here is a go or no-go call, and no operator figure was published for this attempt.