Intasat

Class: Technology. Type: Communications. Destination: Sun Synchronous Orbit. Nation: Spain. Agency: INTA.

Spanish communications satellite.

Typical orbit: 1439 km x 1457 km at 102 degrees inclination. Mass: 20 kg (44 lb). Associated Launch Vehicle: Delta 2000.

Intasat Chronology

1974 November 15 - Intasat 1 - Launch Site: Vandenberg. Launch Vehicle: Delta 2000. Mass: 20 kg (44 lb). Perigee: 1,442 km (896 mi). Apogee: 1,459 km (906 mi). Inclination: 101.80 deg. Period: 114.90 min.

Bibliography and Further Reading

USAF Satellite Database, USAF Institute of Technology, 1995. Accessed at: ftp://archive.afit.af.mil/pub/space/.

McDowell, Jonathan, Jonathan's Space Home Page, Harvard University, 1997-present. Jonathan McDowell's complete on-line listing of all objects orbited and over 20,000 rocket launches Accessed at: http://www.planet4589.org/jsr.html.

Krebs, Gunter, Gunter's Space Page, University of Frankfurt, 1996. Accessed at: http://www.skyrocket.de/space.

JPL Mission and Spacecraft Library, Jet Propulsion Laboratory, 1997. Accessed at: http://msl.jpl.nasa.gov/home.html.

McDowell, Jonathan, Launch Log, October 1998. Jonathan McDowell's complete on-line listing of all objects orbited since Sputnik. Accessed at: http://hea-www.harvard.edu/~jcm/space/log/launch.html.

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© Mark Wade, 1997 - 2007 except where otherwise noted.

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