Also habe ich diesen Artikel gerade gelesen

    https://bohring.substack.com/p/the-story-of-interstellar-comet-3iatlas

    Briefing über den neu entdeckten Kometen 3i/Atlas. Dieser Artikel (schauen Sie sich einmal einmal an) nicht erklären, wie wir wissen, dass solche Objekte interstellar sind. Könnte mir das bitte jemand erklären?

    https://i.redd.it/ucj177eqhlcf1.gif

    How do we know 3I/ATLAS is an interstellar object?
    byu/No-Preparation7618 inspace

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    6 Kommentare

    1. Generally, Direction its coming from, velocity, and trajectory.

      Typically objects that originate from within the solar system, specifically the oort cloud where normal Comets come from won’t have velocity to escape the gravity of the Sun.

    2. TLDR: it’s going too fast to orbit the sun and on the wrong type of trajectory to have originated from a solar orbit, and since the equations that govern these things are known we know the math doesn’t work for anything but interstellar

    3. Easiest way to tell is its velocity. It’s traveling way faster than the escape velocity of the solar system (68 km/s vs 42 km/s), which means it’s not gravitationally bound to the sun

    4. triffid_hunter on

      https://en.wikipedia.org/wiki/Specific_orbital_energy exceeds zero and https://en.wikipedia.org/wiki/Orbital_eccentricity is greater than 1.

      Took astronomers a little bit of time to discern this though – it’s easy to measure angular velocity across our sky, but rather trickier to get a proper position and velocity vector in the reference frame of sun, [ecliptic](https://en.wikipedia.org/wiki/Ecliptic#Plane_of_the_Solar_System), and [FPA](https://en.wikipedia.org/wiki/First_point_of_Aries) necessitating many different measurements of position over some time to narrow down the orbital parameters.

    5. AuroraStarM on

      The „orbit“ of that object has an eccentricity of 6.1 (hyperbolic). To orbit the sun, it would have to be smaller than 1: https://en.m.wikipedia.org/wiki/Orbital_eccentricity

      The eccentricity (e) tells you how much the shape of the orbit deviates from a perfect circle (e = 0). Elliptical orbits have an eccentricity between 0 and 1, where exactly 1 is a parabola.

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