Analysis of the orbits of Titan, Hyperion, and Iapetus by numerical integration

Statistics – Computation

Scientific paper

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Hyperion, Iapetus, Numerical Integration, Orbital Mechanics, Titan, Astrometry, Computational Astrophysics, Least Squares Method, Saturn (Planet), Planets, Satellites, Orbits, Titan, Hyperion, Iapetus, Parameters, Numerical Methods, Astronomy, Celestial Mechanics, Saturn, Techniques, Earth-Based Observations

Scientific paper

The orbits of Titan, Hyperion and Iapetus have been generated by numerical integration and fitted to micrometric observations made in the period of 1874-1923. The least-squares fitting process yields a good determination of the mass ratio Titan/Saturn (2.36651 + or - 0.00028) x 10 to the -4th. The numerical integration has an accurate scale, determined by the value adopted for the mass of Saturn, and so it is a useful means of showing scale errors of the observations. The observations of the angular separation from Saturn were found to be particularly prone to error, being systematically large by about 0.5 arcsec.

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