The space charge region surrounding a highly charged, electron collecting,
spacecraft moving in the ionospheric plasma, can be divided into an inner z
one (close to the spacecraft), where electron collection is isotropic with
respect to the magnetic-field direction, and an outer zone where the electr
ons are mainly collected along magnetic field lines. In this paper we outli
ne a theory to obtain the current voltage characteristic of such a positive
satellite. It is shown that the theoretical results compare very favorably
with the experimental data obtained by the TSS-1R mission.