Launch success.
H3-22 · Navigation


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.
First upwards movement of the rocket
The solid rocket boosters are separated from the launcher.
Separation of the payload fairing
Cut-off of the main engine
Separation of the second stage from the first
First start of the second engine
First cut-off of the second engine
Second start of the second engine
Second cut-off of the second engine
Final deployment of the payload from the rocket
Activity appears when ORBITAL observes a change between source records. No historical events are invented.
Launch success.
Spacecraft separation.
Liftoff.
Official Webcast by JAXA | 宇宙航空研究開発機構 has started
Refined launch window.
Delayed to NET August 10 UTC due to launch site weather.
Rescheduled for NET August 9 UTC.
Delayed due to launch site weather (effects of Typhoon Dolphin).
NET August 6 UTC.
Delayed to TBD due to previous H3 launch failure.
GO for launch.
NET 2025.
No changes recorded
Changes are recorded when ORBITAL retrieves data. The detection time may differ from the time the source changed its information.
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.
Michibiki 7 (QZS-7)
Payload details are described in the mission overview. No independently structured payload manifest or payload mass has been provided by the source.
Yoshinobu Launch Complex LP-2
Tanegashima Space Center, Japan
Official mission broadcast. Stream availability is controlled by the provider.
Source links and confidence are preserved with each mission. Official updates take priority when verified.
Mission photographs are provided by the original sources. Their rights remain with their creators; consult the source before reusing an image.