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A preliminary analysis of the orbit of the Mars Trojan asteroid (5261) EurekaObservations and results of orbit determination of the first known Mars Trojan asteroid (5261) Eureka are presented. We have numerically calculated the evolution of the orbital elements, and have analyzed the behavior of the motion during the next 2 Myr. Strong perturbations by planets other than Mars seem to stabilize the eccentricity of the asteroid by stirring the high order resonances present in the elliptic restricted problem. As a result, the orbit appears stable at least on megayear timescales. The difference of the mean longitudes of Mars and Eureka and the semimajor axis of the asteroid form a pair of variables that essentially behave in an adiabatic manner, while the evolution of the other orbital elements is largely determined by the pertubations due to other planets.
Document ID
19950031859
Acquisition Source
Legacy CDMS
Document Type
Reprint (Version printed in journal)
External Source(s)
Authors
Mikkola, Seppo
(Turku Univ. Observatory, Tuorla, Finland)
Innanen, Kimmo
(York Univ. Toronto, Ontario, Canada)
Muinonen, Karri
(Lowell Observatory, Flagstaff, AZ United States)
Bowell, Edward
(Lowell Observatory, Flagstaff, AZ United States)
Date Acquired
August 16, 2013
Publication Date
January 1, 1994
Publication Information
Publication: Celestial Mechanics and Dynamical Astronomy
Volume: 58
Issue: 1
ISSN: 0923-2958
Subject Category
Astrophysics
Accession Number
95A63458
Funding Number(s)
CONTRACT_GRANT: NAGW-1470
Distribution Limits
Public
Copyright
Other

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