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  2. Orbit determination - Wikipedia

    en.wikipedia.org/wiki/Orbit_determination

    The basic orbit determination task is to determine the classical orbital elements or Keplerian elements, ,,,,, from the orbital state vectors [,], of an orbiting body with respect to the reference frame of its central body. The central bodies are the sources of the gravitational forces, like the Sun, Earth, Moon and other planets.

  3. Gauss's method - Wikipedia

    en.wikipedia.org/wiki/Gauss's_method

    NOTE: Gauss's method is a preliminary orbit determination, with emphasis on preliminary. The approximation of the Lagrange coefficients and the limitations of the required observation conditions (i.e., insignificant curvature in the arc between observations, refer to Gronchi [ 2 ] for more details) causes inaccuracies.

  4. 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.

  5. TRACE (computer program) - Wikipedia

    en.wikipedia.org/wiki/TRACE_(computer_program)

    TRACE is a high-precision orbit determination and orbit propagation program. It was developed by The Aerospace Corporation in El Segundo, California. An early version ran on the IBM 7090 computer in 1964. [1] The Fortran source code can be compiled for any platform with a Fortran compiler.

  6. Atomic orbital - Wikipedia

    en.wikipedia.org/wiki/Atomic_orbital

    The shapes of the first five atomic orbitals are 1s, 2s, 2p x, 2p y, and 2p z.The two colors show the phase or sign of the wave function in each region. Each picture is domain coloring of a ψ(x, y, z) function which depends on the coordinates of one electron.

  7. Lambert's problem - Wikipedia

    en.wikipedia.org/wiki/Lambert's_problem

    In celestial mechanics, Lambert's problem is concerned with the determination of an orbit from two position vectors and the time of flight, posed in the 18th century by Johann Heinrich Lambert and formally solved with mathematical proof by Joseph-Louis Lagrange. It has important applications in the areas of rendezvous, targeting, guidance, and ...

  8. Category:Orbits - Wikipedia

    en.wikipedia.org/wiki/Category:Orbits

    Orbit determination; Orbit equation; Orbital decay; Orbital eccentricity; Orbital elements; Orbital inclination; Orbital node; Orbital shell (spaceflight) Orbital speed; Orbital state vectors; Orbiting body

  9. Extended Hückel method - Wikipedia

    en.wikipedia.org/wiki/Extended_Hückel_method

    A program for the extended Hückel method is YAeHMOP which stands for "yet another extended Hückel molecular orbital package". [10] YAeHMOP has also been merged with the Avogadro open-source molecular editor and visualizer to enable calculations directly from the Avogadro graphical user interface for materials that are periodic in one, two, or ...