GOES-3 was built by Ford Aerospace, and was based on the satellite bus developed for the SMS programme.[8] At launch it had a mass of 627 kilograms (1,382 lb).[2]
The launch successfully placed GOES-C into a geostationary transfer orbit, from which it raised itself to geostationary orbit using an onboard SVM-5 apogee motor. Its insertion into geosynchronous orbit occurred at 03:22 on 17 June.[1]
GOES-C underwent on-orbit testing, and was subsequently redesignated GOES-3. It replaced GOES 1 in service, and was initially operated at 135° West. In 1981, it was moved to 90° West, arriving in 1982, before departing again in 1984. In 1985 it arrived back at 135° West. In 1987 it was moved to 129° West, where it operated until it became unusable for meteorological studies in 1989.
^ abMcDowell, Jonathan. "Index". Geostationary Orbit Catalog. Jonathan's Space Page. Archived from the original on April 6, 2010. Retrieved August 13, 2009.
^ abcWade, Mark. "GOES". Encyclopedia Astronautica. Archived from the original on February 21, 2002. Retrieved August 13, 2009.
Payloads are separated by bullets ( · ), launches by pipes ( | ). Crewed flights are indicated in underline. Uncatalogued launch failures are listed in italics. Payloads deployed from other spacecraft are denoted in (brackets).