RecapLAUNCH SUCCESSFULLive

Martian Moons eXploration

H3-⁠24Tanegashima, Japan

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JAXA

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JAXA

Mission

H3-⁠24 launched Martian Moons eXploration from Yoshinobu Launch Complex LP-⁠2 at Tanegashima Space Center, Japan.

Before the flight

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.

Launched
Tue 04:41:03 UTC+9 at the pad
Rocket
H3-⁠24MHI
Destination
Mars Orbit
Launch site
Yoshinobu Launch Complex LP-⁠2, Tanegashima, Japan3rd launch from this pad in 202670 days after the last

1h11min

Mission duration

3rd

MHI launch of 2026

Flight

From liftoff to orbit

  1. Yoshinobu Launch Complex LP-2
  2. LiftoffT+00:00:00
  3. Stage separationT+00:04:59
  4. SECOT+00:10:40
  1. Yoshinobu Launch Complex LP-2
  2. LiftoffT+00:00:00
  3. Stage separationT+00:04:59
  4. SECOT+00:10:40
  1. Yoshinobu Launch Complex LP-2
  2. LiftoffT+00:00:00
  3. Stage separationT+00:04:59
  4. SECOT+00:10:40
Schematic, not to scale. Tap a moment for more.Point at a moment for more.

All times approximate, in your time zone (CEST)Timeline: The Space Devs

  1. T plus 0 secondsLiftoff
  2. T plus 1 minute 56 secondsBoosters Separation
  3. T plus 3 minutes 17 secondsFairing Separation, Upper stage
  4. T plus 4 minutes 52 secondsMECO
  5. T plus 4 minutes 59 secondsStage 2 Separation
  6. T plus 5 minutes 12 secondsSES-⁠1, Upper stage
  7. T plus 10 minutes 40 secondsSECO-⁠1, Upper stage
  8. T plus 1 hour 3 minutesSES-⁠2, Upper stage
  9. T plus 1 hour 10 minutesSECO-⁠2, Upper stage
  10. T plus 1 hour 11 minutesPayload Separation

H3-24

MHI2 launches since October 2025, 2 successful

63m

Height

5.3m

Diameter

12.1MN

Thrust at liftoff

7.9t

Payload to geostationary transfer orbit

About H3-24

The H3 Launch Vehicle is a Japanese expendable launch system. Each H3 booster configuration has a two-digit and a letter designation that indicates the features of that configuration. The first digit represents the number of LE-⁠9 engines on the main stage, either “2” or “3”. The second digit indicates the number of SRB-⁠3 solid rocket boosters attached to the base of the rocket, and can be “0”, “2” or “4”. All layouts of solid boosters are symmetrical. The letter in the end shows the length of the payload fairing, either short “S” or long “L”. For example, an H3-⁠24L has two engines, four solid rocket boosters, and a long fairing, whereas an H3-⁠30S has three engines, no solid rocket boosters, and a short fairing.

Orbit estimated from CelesTrak’s elementsMeasured trackSpaceX’s predicted path

In orbit now

The crewed stations and Hubble, once around the Earth every 92 to 94 minutes

SpacecraftAltitudeSpeed
ISSDocked: Soyuz MS-⁠29, Crew-⁠13In Earth’s shadow430km27,561km/h
TiangongDocked: Shenzhou-⁠23In sunlight385km27,652km/h
HubbleIn sunlight477km27,461km/h

Estimated for from CelesTrak’s orbital elements, up to 33 h old.

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