Published May 2011 | Version v1
Journal article

ORBITS OF NEAR-EARTH ASTEROID TRIPLES 2001 SN263 AND 1994 CC: PROPERTIES, ORIGIN, AND EVOLUTION

  • 1. Department of Physics and Astronomy, University of California Los Angeles, Los Angeles, CA 90095 (United States)
  • 2. Jet Propulsion Laboratory, California Institute of Technology, Pasadena, CA 91109 (United States)
  • 3. Arecibo Observatory, National Astronomy and Ionosphere Center, Arecibo, PR 00612 (Puerto Rico)

Description

Three-body model fits to Arecibo and Goldstone radar data reveal the nature of two near-Earth asteroid triples. The triple-asteroid system 2001 SN263 is characterized by a primary of ∼1013 kg, an inner satellite ∼1% as massive orbiting at ∼3 primary radii in ∼0.7 days, and an outer satellite ∼2.5% as massive orbiting at ∼13 primary radii in ∼6.2 days. 1994 CC is a smaller system with a primary of mass ∼2.6 x1011 kg and two satellites ∼2% and ∼<1% as massive orbiting at distances of ∼5.5 and ∼19.5 primary radii. Their orbital periods are ∼1.2 and ∼8.4 days. Examination of resonant arguments shows that the satellites are not currently in a mean-motion resonance. Precession of the apses and nodes are detected in both systems (2001 SN263 inner body: dpiv/dt ∼ 1.1 deg day-1; 1994 CC inner body: dpiv/dt∼ -0.2 deg day-1), which is in agreement with analytical predictions of the secular evolution due to mutually interacting orbits and primary oblateness. Nonzero mutual inclinations between the orbital planes of the satellites provide the best fits to the data in both systems (2001 SN263: ∼ 14 deg; 1994 CC: ∼16 deg). Our best-fit orbits are consistent with nearly circular motion, except for 1994 CC's outer satellite which has an eccentric orbit of e ∼ 0.19. We examine several processes that can generate the observed eccentricity and inclinations, including the Kozai and evection resonances, past mean-motion resonance crossings, and close encounters with terrestrial planets. In particular, we find that close planetary encounters can easily excite the eccentricities and mutual inclinations of the satellites' orbits to the currently observed values.

Availability note (English)

Available from http://dx.doi.org/10.1088/0004-6256/141/5/154

Additional details

Identifiers

Publishing Information

Journal Title
Astronomical Journal (New York, N.Y. Online)
Journal Volume
141
Journal Issue
5
Journal Page Range
[15 p.]
ISSN
1538-3881

INIS

Country of Publication
United States
Country of Input or Organization
International Atomic Energy Agency (IAEA)
INIS RN
43060695
Subject category
S79: ASTROPHYSICS, COSMOLOGY AND ASTRONOMY;
Descriptors DEI
ASTEROIDS; INCLINATION; ORBITS; PLANETS; SATELLITES; STAR EVOLUTION; THREE-BODY PROBLEM
Descriptors DEC
EVOLUTION; MANY-BODY PROBLEM