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  2. Two-body problem in general relativity - Wikipedia

    en.wikipedia.org/wiki/Two-body_problem_in...

    In 1859, Urbain Le Verrier discovered that the orbital precession of the planet Mercury was not quite what it should be; the ellipse of its orbit was rotating (precessing) slightly faster than predicted by the traditional theory of Newtonian gravity, even after all the effects of the other planets had been accounted for. [4]

  3. Orbital period - Wikipedia

    en.wikipedia.org/wiki/Orbital_period

    Inversely, for calculating the distance where a body has to orbit in order to have a given orbital period T: a = G M T 2 4 π 2 3 {\displaystyle a={\sqrt[{3}]{\frac {GMT^{2}}{4\pi ^{2}}}}} For instance, for completing an orbit every 24 hours around a mass of 100 kg , a small body has to orbit at a distance of 1.08 meters from the central body's ...

  4. Orbital mechanics - Wikipedia

    en.wikipedia.org/wiki/Orbital_mechanics

    The square of a satellite's orbital period is proportional to the cube of its average distance from the planet. Without applying force (such as firing a rocket engine), the period and shape of the satellite's orbit will not change.

  5. Kepler's laws of planetary motion - Wikipedia

    en.wikipedia.org/wiki/Kepler's_laws_of_planetary...

    This captures the relationship between the distance of planets from the Sun, and their orbital periods. Kepler enunciated in 1619 [ 16 ] this third law in a laborious attempt to determine what he viewed as the " music of the spheres " according to precise laws, and express it in terms of musical notation. [ 25 ]

  6. Two-body problem - Wikipedia

    en.wikipedia.org/wiki/Two-body_problem

    In classical mechanics, the two-body problem is to calculate and predict the motion of two massive bodies that are orbiting each other in space. The problem assumes that the two bodies are point particles that interact only with one another; the only force affecting each object arises from the other one, and all other objects are ignored.

  7. Orbital eccentricity - Wikipedia

    en.wikipedia.org/wiki/Orbital_eccentricity

    where E is the total orbital energy, L is the angular momentum, m rdc is the reduced mass, and the coefficient of the inverse-square law central force such as in the theory of gravity or electrostatics in classical physics: = (is negative for an attractive force, positive for a repulsive one; related to the Kepler problem)

  8. Elliptic orbit - Wikipedia

    en.wikipedia.org/wiki/Elliptic_orbit

    An elliptical orbit is depicted in the top-right quadrant of this diagram, where the gravitational potential well of the central mass shows potential energy, and the kinetic energy of the orbital speed is shown in red. The height of the kinetic energy decreases as the orbiting body's speed decreases and distance increases according to Kepler's ...

  9. General relativity - Wikipedia

    en.wikipedia.org/wiki/General_relativity

    Orbital decay for PSR J0737−3039: time shift (in s), tracked over 16 years (2021). [96] According to general relativity, a binary system will emit gravitational waves, thereby losing energy. Due to this loss, the distance between the two orbiting bodies decreases, and so does their orbital period.