FTV-1132 was operated in a low Earth orbit, with a perigee of 288 kilometres (179 mi), an apogee of 670 kilometres (420 mi), 82.8 degrees of inclination, and a period of 94.2 minutes. The satellite had a mass of 1,150 kilograms (2,540 lb), and was equipped with a frame camera with a focal length of 76 millimetres (3.0 in), which had a maximum resolution of 140 metres (460 ft). Images were recorded onto 127-millimetre (5.0 in) film, and returned in a Satellite Recovery Vehicle, before the satellite ceased operations. The Satellite Recovery Vehicle used by FTV-1132 was SRV-600. Following atmospheric reentry, SRV-600 was to have been collected in mid-air by a Fairchild C-119J Flying Boxcar aircraft, however when this was attempted the parachute separated from the spacecraft, causing the capsule to fall into the sea. FTV-1132 decayed from orbit on 26 October 1964.
Payloads are separated by bullets ( · ), launches by pipes ( | ). Manned flights are indicated in bold text. Uncatalogued launch failures are listed in italics. Payloads deployed from other spacecraft are denoted in brackets.
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