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  2. Lagrange point - Wikipedia

    en.wikipedia.org/wiki/Lagrange_point

    There are five Lagrange points for the Sun–Earth system, and five different Lagrange points for the Earth–Moon system. L 1, L 2, and L 3 are on the line through the centers of the two large bodies, while L 4 and L 5 each act as the third vertex of an equilateral triangle formed with the centers of the two large bodies.

  3. List of objects at Lagrange points - Wikipedia

    en.wikipedia.org/wiki/List_of_objects_at...

    Sun–Earth L 2: ESA, NASA Launched on 1 July 2023, arrived at L 2 point on 28 July 2023. Currently in testing phase as of September 2023. [42] Aditya-L1: Sun–Earth L 1: ISRO: Launched on 2 September 2023 [43] and was successfully inserted into an orbit about Sun-Earth L 1 point on 6 January 2024. [44] Chang'e 6 Service Module: Sun–Earth L ...

  4. Interplanetary Transport Network - Wikipedia

    en.wikipedia.org/wiki/Interplanetary_Transport...

    Although the forces balance at these points, the first three points (the ones on the line between a certain large mass, e.g. a star, and a smaller, orbiting mass, e.g. a planet) are not stable equilibrium points. If a spacecraft placed at the Earth–Moon L 1 point is given even a slight nudge away from the equilibrium point, the spacecraft's ...

  5. Sun-synchronous orbit - Wikipedia

    en.wikipedia.org/wiki/Sun-synchronous_orbit

    An orbit will be Sun-synchronous when the precession rate ρ = ⁠ dΩ / dt ⁠ equals the mean motion of the Earth about the Sun n E, which is 360° per sidereal year (1.990 968 71 × 10 −7 rad/s), so we must set n E = ⁠ ΔΩ E / T E ⁠ = ρ = ⁠ ΔΩ / T ⁠, where T E is the Earth orbital period, while T is the period of the spacecraft ...

  6. Halo orbit - Wikipedia

    en.wikipedia.org/wiki/Halo_orbit

    A halo orbit is a periodic, three-dimensional orbit associated with one of the L 1, L 2 or L 3 Lagrange points in the three-body problem of orbital mechanics.Although a Lagrange point is just a point in empty space, its peculiar characteristic is that it can be orbited by a Lissajous orbit or by a halo orbit.

  7. Earth's orbit - Wikipedia

    en.wikipedia.org/wiki/Earth's_orbit

    One complete orbit takes 365.256 days (1 sidereal year), during which time Earth has traveled 940 million km (584 million mi). [2] Ignoring the influence of other Solar System bodies, Earth's orbit, also called Earth's revolution, is an ellipse with the Earth–Sun barycenter as one focus with a current eccentricity of 0.0167. Since this value ...

  8. Aditya-L1 - Wikipedia

    en.wikipedia.org/wiki/Aditya-L1

    It is orbiting at about 1.5 million km from Earth in a halo orbit around the Lagrange point 1 (L1) between the Earth and the Sun, where it will study the solar atmosphere, solar magnetic storms, and their impact on the environment around the Earth. [7] It is the first Indian mission dedicated to observe the Sun. Nigar Shaji is the project's ...

  9. Libration point orbit - Wikipedia

    en.wikipedia.org/wiki/Libration_point_orbit

    The James Webb Space Telescope (JWST) is in a libration point orbit around the L2 Lagrange point of the Sun, and Earth-Moon barycenters. [2] [3] Because libration point orbits are quasiperiodic, the telescope must make frequent small burns to maintain proximity to the L2 point, as part of orbital station keeping, limiting the lifespan of the ...