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An acquisition Sun sensor, a cruise Sun sensor, a Canopus star tracker and an inertial reference unit consisting of six gyroscopes allowed three-axis stabilization.
Two accelerometers were also on board.
Communications were accomplished through a S-band ( 2. 3 GHz ) transmitter and two TWTAs.
An X band downlink was also added specifically for radio science and to conduct communications experiments.
Uplink was via S band A two-axis steerable high-gain parabolic dish antenna with a diameter of approximately 1. 5 m was attached at one edge of the orbiter base, and a fixed low-gain antenna extended from the top of the bus.
Two tape recorders were each capable of storing 1280 megabits.
A 381-MHz relay radio was also available.

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