H-2A
| Status | Retired |
|---|---|
| Country | Japan |
| Manufacturer | Mitsubishi Heavy Industries |
| Number of orbital launches | 50 |
| First launch | 2001-08-29 |
| Last launch | 2025-06-28 |
Launches by year:
Latest launches:
| Launch date | Launch site | Rocket / Variant | Payload | Notes | Status |
|---|---|---|---|---|---|
| 2025-06-28 | Tanegashima | H-2A 202 | GOSAT-GW | success | |
Final H-2A launch | |||||
| 2024-09-26 | Tanegashima | H-2A 202 | IGS Radar 8 | success | |
| 2024-01-12 | Tanegashima | H-2A 202 | IGS Optical 8 | success | |
| 2023-09-06 | Tanegashima | H-2A 202 | XRISM / SLIM | B | success |
| 2023-01-26 | Tanegashima | H-2A 202 | IGS Radar 7 | success | |
| 2021-12-22 | Tanegashima | H-2A 204 | Inmarsat 6 F1 | success | |
| 2021-10-26 | Tanegashima | H-2A 202 | QZS-1R (Michibiki 1R) | success | |
| 2020-11-29 | Tanegashima | H-2A 202 | JDRS 1 | success | |
| 2020-07-19 | Tanegashima | H-2A 202 | Al Amal | B | success |
| 2020-02-09 | Tanegashima | H-2A 202 | IGS Optical 7 | success | |
| + 40 more... | |||||
Variants:
(This section is under construction)H-2A 202
| First launch | 2001-08-29 |
|---|---|
| Boosters | 2 |
Payload capacity:
| LEO | 10000 kg to 250 km / 30 deg |
|---|
H-2A 2024
| First launch | 2002-02-04 |
|---|
H-2A 2022
| First launch | 2005-02-26 |
|---|
H-2A 204
| First launch | 2006-12-18 |
|---|---|
| Boosters | 4 |
| Mass | 445 t |
| Height | 53 m |
