Earth Orbit Orbital altitude approx. 550km Inclination approx. 35.00 degrees Weight approx. Orbit Period approx. The major mission of ETS-VII is to acquire the basic technologies of rendezvous docking and space roboties which are essential to future space activities such as retrieval, resupply and exchange of equipment on orbit.
Some data are on line for electronic access.
Information on the current status of the instruments on board from the investigators will be most welcomed. This URL also enables executing several codes related to the orbits of many geocentric science payload spacecraft.