Official name VEP
Alternative name Myojo
Cospar ID 1994-007B
Norad ID 22979
Launch date 1994-02-03
Launch site TNSTA
Launch vehicle H-2
Country/Organization Japan
Type application Vehicle evaluation
Operator NASDA
RCS size LARGE
Decay date ON ORBIT
Period (min) 637.55
Inclination (deg) 28.28
Perigee (km) 379
Apogee (km) 35940
Eccentricity 0.979129381315565
Mean motion (revs. per day) 2.25864638067603
Semi-Major axis (km) 24537.635
Raan (deg) 155.2066
Arg of perigee (deg) 76.0246
Shape Box
Mass (kg) 2378.59
Height (m) 3
Width (m) 2
Depth (m) 3
Span (m^2) 3
Contractors NASDA
Power Batteries

The Vehicle Evaluation Payload (VEP), renamed Myojo after launch, was a Japanese spacecraft that was launched by an H-2 rocket from the Tanegashima Tanegashima launch site.

It provided a ranging function as well as functions to measure the acceleration and deformation, in order to confirm the accuracy of the H-2 rocket orbit injection and understand the environment of the payload equipment. It remained intentionally attached to the second stage of the H-2 launch vehicle. It carried the OREX reentry experiment on top, which was deployed in orbit.

Satellite COSPAR Date LS Launch Vehicle Remarks
VEP 1994-007B 1994-02-03 TNSTA H-2 with OREX