🚀Launchpad

Payload / Mission

LRE

Type
Planetary Science
Orbit
Geosynchronous Transfer Orbit (GSTO)

The H-IIA Launch Vehicle No.1 (H-IIA/F1) was launched at 4:00 p.m. on August 29, 2001, Japan Standard Time, from Tanegashima Space Center. The launch vehicle was successfully lifted off with its flight azimuth of 90 degrees. The H-IIA Launch Vehicle No.1 flied normally, and the second stage was successfully injected into the geostationary transfer orbit. The separation of the Laser Ranging Equipment (LRE) was confirmed about 39 minutes and 47 seconds after the lift-off.