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Class: Technology. Nation: Japan. Agency: Japan(Lambda 4S 5).
Engineering test for the launching of scientific satellites. Injection point 29.7 N, 145.8 E.
Total Mass: 12 kg.
11 February 1970
Ohsumi 5 Launch Site: Kagoshima . Launch Vehicle: L-4S. Mass: 12 kg. Perigee: 323 km. Apogee: 2,440 km. Inclination: 31.0 deg.
Engineering tests. Engineering test for the launching of scientific satellites. Injection point 29.7 N, 145.8 E
- 2 - McDowell, Jonathan, The United Nations Registry of Space Objects, Harvard University, 1997. HTML when accessed: http://hea-www.harvard.edu/QEDT/jcm/space/un/un.html
- 6 - JPL Mission and Spacecraft Library, Jet Propulsion Laboratory, 1997. HTML when accessed: http://msl.jpl.nasa.gov/home.html
- 279 - McDowell, Jonathan, Launch Log, October 1998. HTML when accessed: http://hea-www.harvard.edu/~jcm/space/log/launch.html
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Last update 12 March 2001.
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© Mark Wade, 2001 .