A balloon satellite, sometimes referred to as a "satelloon", is inflated with gas after it has been put into orbit.
Echo 1 and Echo 2 balloon satellites
The first flying body of this type was Echo 1, which was launched into a high orbit on August 12, 1960, by the United States. It originally had a spherical shape measuring , with a thin metal-coated plastic shell made of Mylar. It served for testing as a "passive" communication and geodetic satellite.
One of the first radio contacts using the satellite was successful at a distance of nearly (between the east coast of the US and California). By the time Echo 1 burned up in 1968, the measurements of its orbit by several dozen earth stations had improved our knowledge of the precise shape of the planet by nearly a factor of ten.
Its successor was the similarly built Echo 2 (1964 to about 1970). This satellite circled the Earth about lower, not at an angle of 47° like that of Echo 1, but in a polar orbit with an average angle of 81°. This enabled radio contact and measurements to be made at higher latitudes. Taking part in the Echo orbit checks to analyze disturbances in its orbit and in the Earth's gravitational field were thirty to fifty professional earth stations, as well as around two hundred amateur astronomers across the planet in "Moonwatch" stations; these contributed around half of all sightings.
Range of radio waves, visibility
The Pythagorean theorem allows us to calculate easily how far a satellite is visible at such a great height. It can be determined that a satellite in a orbit rises and sets when the horizontal distance is . However, the atmosphere causes this figure to vary slightly. Thus if two radio stations are apart and the satellite's orbit goes between them, they may be able to receive each other's reflected radio signals if the signals are strong enough.
Optical visibility is, however, lower than that of radio waves, because
the satellite must be illuminated by the sun
the observer needs a dark sky (that is, he must be in the Earth's own shadow on the planet's twilight or night side) the brightness of a sphere depends on the angle between the incident light and the observer (see phases of the moon) the brightness of a sphere is much reduced as it approaches the horizon, as atmospheric extinction swallows up as much as 90% of the light
Despite this there is no problem observing a flying body such as Echo 1 for precise purposes of satellite geodesy, down to a 20° elevation, which corresponds to a distance of . In theory this means that distances of up to between measuring points can be "bridged", and in practice this can be accomplished at up to .
For visual and photographic observation of bright satellites and balloons, and regarding their geodetic use, see Echo 1 and Pageos for further information.
Other balloon satellites
For special testing purposes two or three satellites of the Explorer series were constructed as balloons (possibly Explorer 19 and 38).
Echo 1 was an acknowledged success of radio engineering, but the passive principle of telecommunications (reflection of radio waves on the balloon's surface) was soon replaced by active systems. Telstar 1 (1962) and Early Bird (1965) were able to transmit several hundred audio channels simultaneously in addition to a television program exchanged between continents.
Satellite geodesy with Echo 1 and 2 was able to fulfill all expectations not only for the planned 2–3 years, but for nearly 10 years. For this reason NASA soon planned the launch of the even larger balloon Pageos. The name is from "passive geodesic satellite", and sounds similar to "Geos", a successful active electronic satellite from 1965.
Pageos and the global network
Pageos was specially launched for the "global network of satellite geodesy", which occupied about 20 full-time observing teams all over the world until 1973. All together they recorded 3000 usable photographic plates from 46 tracking stations with calibrated all-electronic BC-4 cameras (1:3 / focal length ). From these images they were able to calculate the stations' position three-dimensionally with a precision of about . The coordinator of this project was Professor Hellmut Schmid, from the ETH Zurich.
Three stations of the global network were situated in Europe: Catania in Sicily, Hohenpeißenberg in Bavaria and Tromsø in northern Norway. For the completion of the navigational network exact distance measurements were needed; these were taken on four continents and across Europe with a precision of per kilometer.