H3-22 | Michibiki 5 (QZS-5)
03/02/2025 Ultimo aggiornamento
President: Seiji Izumisawa Amministratore
To Be Determined Status

H3-22 | Michibiki 5 (QZS-5)

Tanegashima Space Center, Japan

Orbital Launch Attempt Count: 7100

Location Launch Attempt Count: 100

Pad Launch Attempt Count: 19

Agency Launch Attempt Count: 59

Launch Designator:

Net Precision: Year

Weather Concerns:

Fail Reason:

Flightclub URL:

Pad Turnaround: P61D

Programma

Pad

H-IIB 304 liftoff from LP-2 (HTV-3)
Yoshinobu Launch Complex LP-2

The Tanegashima Space Center is the largest rocket-launch complex in Japan. It is located on the southeastern tip of Tanegashima, an island located south of Kyushu, an island and region and Japan. It was established in 1969 when the National Space Development Agency of Japan (NASDA) was formed, and is now run by JAXA. The activities that take place at TNSC include assembly, testing, launching, and tracking satellites, as well as rocket engine firing tests.

Rocket

H3-22 liftoff (ALOS-3)
H3-22

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.

Full Name: H3-22

Maiden Flight: 2023-03-07

Total Launch Count: 5

Successful Launches: 4

Failed Launches: 1

Mission

Mission Name: Michibiki 5 (QZS-5)

Type: Navigation

Description: 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.

Orbit: Geosynchronous Transfer Orbit

Updates

Cosmic_Penguin

Cosmic_Penguin

2024-01-09T14:30:05Z
https://www8.cao.go.jp/space/comittee/dai108/siryou2_2.pdf

Tweaked approximate launch date per launch manifest (P.129 of source).