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  2. Orbit modeling - Wikipedia

    en.wikipedia.org/wiki/Orbit_modeling

    Orbit modeling is the process of creating mathematical models to simulate motion of a massive body as it moves in orbit around another massive body due to gravity.Other forces such as gravitational attraction from tertiary bodies, air resistance, solar pressure, or thrust from a propulsion system are typically modeled as secondary effects.

  3. Orbital state vectors - Wikipedia

    en.wikipedia.org/wiki/Orbital_state_vectors

    Orbital position vector, orbital velocity vector, other orbital elements. In astrodynamics and celestial dynamics, the orbital state vectors (sometimes state vectors) of an orbit are Cartesian vectors of position and velocity that together with their time () uniquely determine the trajectory of the orbiting body in space.

  4. Two-body problem - Wikipedia

    en.wikipedia.org/wiki/Two-body_problem

    The most prominent example of the classical two-body problem is the gravitational case (see also Kepler problem), arising in astronomy for predicting the orbits (or escapes from orbit) of objects such as satellites, planets, and stars. A two-point-particle model of such a system nearly always describes its behavior well enough to provide useful ...

  5. Orbit (dynamics) - Wikipedia

    en.wikipedia.org/wiki/Orbit_(dynamics)

    In mathematics, specifically in the study of dynamical systems, an orbit is a collection of points related by the evolution function of the dynamical system. It can be understood as the subset of phase space covered by the trajectory of the dynamical system under a particular set of initial conditions , as the system evolves.

  6. Clohessy–Wiltshire equations - Wikipedia

    en.wikipedia.org/wiki/Clohessy–Wiltshire_equations

    Suppose a target body is moving in a circular orbit and a chaser body is moving in an elliptical orbit. Let ,, be the relative position of the chaser relative to the target with radially outward from the target body, is along the orbit track of the target body, and is along the orbital angular momentum vector of the target body (i.e., ,, form a right-handed triad).

  7. Co-orbital configuration - Wikipedia

    en.wikipedia.org/wiki/Co-orbital_configuration

    Most of these orbit near Jupiter's Lagrangian points, the traditional Jupiter trojans. As of 2015, there are also 13 Neptune trojans, 7 Mars trojans, 2 Uranus trojans ((687170) 2011 QF 99 and (636872) 2014 YX 49), and 2 Earth trojans (2010 TK 7 and (614689) 2020 XL 5) that are known to exist. No Saturnian trojans have been observed until the ...