Author/Authors :
Shalini and Sokova، نويسنده , , I.A. and Sokov، نويسنده , , E.N. and Roschina، نويسنده , , E.A. and Rastegaev، نويسنده , , D.A and Kiselev، نويسنده , , A.A. and Balega، نويسنده , , Yu.Yu. and Gorshanov، نويسنده , , D.L. and Malogolovets، نويسنده , , E.V. and Dyachenko، نويسنده , , V.V. and Maksimov، نويسنده , , A.F.، نويسنده ,
Abstract :
In this paper we present the orbital elements of Linus satellite of 22 Kalliope asteroid. Orbital element determination is based on the speckle interferometry data obtained with the 6-m BTA telescope operated by SAO RAS. We processed 9 accurate positions of Linus orbiting around the main component of 22 Kalliope between 10 and 16 December, 2011. In order to determine the orbital elements of the Linus we have applied the direct geometric method. The formal errors are about 5 mas. This accuracy makes it possible to study the variations of the Linus orbital elements influenced by different perturbations over the course of time. Estimates of six classical orbital elements, such as the semi-major axis of the Linus orbit a = 1109 ± 6 km, eccentricity e = 0.016 ± 0.004, inclination i = 101° ± 1° to the ecliptic plane and others, are presented in this work.
Keywords :
Orbit Determination , Satellites of asteroids , celestial mechanics , Asteroids
