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Watch the Launch

Michibiki 5 (QZS-5)

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Overview

Destination: Geosynchronous Transfer Orbit
Mission: Navigation

Geosynchronous Transfer Orbit Yoshinobu Launch Complex LP-2 Tanegashima Space Center, Japan

QZSS (Quasi Zenith Satellite System) is a Japanese satellite navigation system operating from inclined, elliptical geosynchronous orbits to achieve optimal high-elevation visibility in urban canyons and mountainous areas. The navigation system objective is to broadcast GPS-interoperable and augmentation signals as well as original Japanese (QZSS) signals from a three-spacecraft constellation. The navigation system objective is to broadcast GPS-interoperable and augmentation signals as well as original Japanese (QZSS) signals from a three-spacecraft constellation in inclined, elliptical geosynchronous orbits.

Updates

Cosmic_Penguin • Dec. 13, 2025, 4 p.m.

Rescheduled for December 17.


Cosmic_Penguin • Dec. 15, 2025, 5:04 a.m.

Tweaked launch window.


Cosmic_Penguin • Dec. 17, 2025, 1:15 a.m.

Tweaked T-0.


Cosmic_Penguin • Dec. 17, 2025, 2:12 a.m.

Hold at T-13 seconds.


Cosmic_Penguin • Dec. 17, 2025, 2:16 a.m.

Scrubbed for the day.


H3-22

Family:
Configuration: 22

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.

See Details
Specifications
  • Stages
    2
  • Length
    63.0 m
  • Diameter
    5.27 m
  • Fairing Diameter
    5.27 m
  • Launch Mass
    ―
  • Thrust
    7542.0 kN
Family
  • Name
    H3-22
  • Family
    ―
  • Variant
    22
  • Alias
    ―
  • Full Name
    H3-22
Payload Capacity
  • Launch Cost
    $50000000
  • Low Earth Orbit
    ―
  • Geostationary Transfer Orbit
    5400.0 kg
  • Direct Geostationary
    ―
  • Sun-Synchronous Capacity
    ―

Mitsubishi Heavy Industries

Mitsubishi Heavy Industries

(MHI)

President: Seiji Izumisawa Founded: 1884 Successes: 56 Failures: 2 Pending: 13

Agency Type:

Mitsubishi Heavy Industries, Ltd. is a Japanese multinational engineering, electrical equipment and electronics company headquartered in Tokyo, Japan. MHI is one of the core companies of the Mitsubishi Group. MHI's products include aerospace components, air conditioners, aircraft, automotive components, forklift trucks, hydraulic equipment, machine tools, missiles, power generation equipment, printing machines, ships and space launch vehicles. Through its defense-related activities, it is the world's 23rd-largest defense contractor measured by 2011 defense revenues and the largest based in Japan.

INFO WIKI
NASASpaceflight

Launch Roundup: Ariane 6, Falcon 9, Atlas V, and Electron launches highlight busy week

Global launch activity is set to surge over the next week, with 13 missions scheduled… The post Launch Roundup: Ariane 6, Falcon 9, Atlas V, and Electron launches highlight busy week appeared first on NASASpaceFlight.com.

Spaceflight Now

H3 rocket suffers upper stage anomaly, fails to correctly deploy navigation satellite

The Dec. 22 launch was the fourth and final flight of an H3 rocket in 2025.

SpaceNews

Japan’s H3 suffers second-stage anomaly, QZS-5 satellite lost

Japan’s flagship H3 rocket suffered an issue with its second stage late Sunday resulting in the loss of the Michibiki 5 (QZS-5) navigation satellite. The post Japan’s H3 suffers second-stage anomaly, QZS-5 satellite lost appeared first on…

SpaceNews

H3 failure linked to payload fairing separation anomaly

An H3 launch failure in December may have been caused by an unusual event that led to the satellite separating from the rocket prematurely. The post H3 failure linked to payload fairing separation anomaly appeared first on SpaceNews.

Arstechnica

Rocket Report: How a 5-ton satellite fell off a booster; will SpaceX and xAI merge?

"We’re seeing remarkable growth year after year."

Tanegashima Space Center, Japan

Yoshinobu Launch Complex LP-2


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