Evolution of e and I oscillations
Inner 4 planets
Eccentricities and inclinations of the four inner planetary orbits in the
beginning and final parts of the integration, N_+1.
(a)-(d): Eccentricities of Mercury, Venus, Earth, and Mars in the beginning
of the integration.
(e)-(h): Inclinations of Mercury, Venus, Earth, and Mars in the beginning
of the integration.
(i)-(l): Eccentricities of Mercury, Venus, Earth, and Mars in the final
of the integration.
(m)-(p): Inclinations of Mercury, Venus, Earth, and Mars in the final
of the integration.
All the elements are reckoned on the solar system invariable plane with
heliocentric origin. The unit of inclinations is degree.
N+1
N+2
N+3
N-1
N-2
N-3
Outer 5 planets
Eccentricities and inclinations of the five outer planetary orbits in the
final parts of the integrations, F_+/-.
(a)-(e): Eccentricities of Jupiter, Saturn, Uranus, Neptune, and Pluto in
the final part of F_- integration.
(f)-(j): Inclinations of Jupiter, Saturn, Uranus, Neptune, and Pluto in
the final part of F_- integration.
(k)-(o): Eccentricities of Jupiter, Saturn, Uranus, Neptune, and Pluto in
the final part of F_+ integration.
(p)-(t): Inclinations of Jupiter, Saturn, Uranus, Neptune, and Pluto in
the final part of F_+ integration.
All the elements are reckoned on the solar system invariable plane with
heliocentric origin.
F+/-
N+1
N+2
N+3
N-1
N-2
N-3
F+/-