In February 1990, contact was re-established with the ESA cometary spa
cecraft, Giotto, but the signal was too weak for telemetry and only Do
ppler data provided information on the status and dynamics of the spac
ecraft. These data showed that the orbit prediction had been accurate
and were used to determine the spacecraft spin-rate. After several bli
nd major reconfigurations of the spacecraft, the Doppler analyses prov
ed that the High-Gain Antenna (HGA) had been despun and an attitude ma
neuver successfully performed. The Doppler change allowed the attitude
to be reconstructed and eventually enabled normal communications via
the HGA. Subsequently, the orbit was regularly determined from Doppler
and range measurements and Giotto made the first ever Earth swing-by
on July 2, 1990.