Nozomi

Success ISAS, M-V

Mission

Robotic Exploration · Helio-N/A

The primary scientific objective of Nozomi program is to study the Martian upper atmosphere with emphasis on its interaction with the solar wind.

What it put in orbit

ObjectTypeOrbitGlobe
NOZOMI (PLANET-B) 1998-041A Payload orbits the Sun
M-V R/B(1) 1998-041B Rocket body re-entered 1998-07-08
M-V DEB 1998-041D Debris re-entered 1998-07-05
M-V DEB 1998-041E Debris re-entered 1998-07-31
M-V R/B(2) 1998-041C Rocket body 1917 × 592196 km · 23.9° Globe

COSPAR ID 1998-041. Orbits from the CelesTrak satellite catalogue (perigee × apogee, inclination).

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