Orbital Element Determination

Orbital Element Determination is the systematic process of deriving the set of orbital elements that uniquely define the trajectory of a celestial body or artificial satellite in space, distinguished by its reliance on observational data and mathematical models to infer the six classical Keplerian parameters or equivalent state vectors.

48

Publications

2K

Citations

103

Authors

68

Institutions

Publications per year

2017–2026

5

Authors

103

  1. DN
    D. Naef

    Observatoire Cantonal de Neuchâtel, Switzerland

    5 publications · 372 citations

    5

    h-index

  2. CP
    C. Perrier

    Centre National de la Recherche Scientifique, France

    5 publications · 372 citations

    5

    h-index

  3. SU
    S. Udry

    University of Geneva, Switzerland

    5 publications · 372 citations

    5

    h-index

  4. JB
    Jean-Luc Beuzit

    Centre National de la Recherche Scientifique, France

    5 publications · 372 citations

    5

    h-index

  5. JP
    J. P. Sivan

    Laboratoire d’Astrophysique de Marseille, France

    5 publications · 372 citations

    5

    h-index

1–5 of 103

Venues

  1. The Astronomical Journal

    AJ · 8 publications · 321 citations

    8

    h-index

  2. Celestial Mechanics and Dynamical Astronomy

    6 publications · 249 citations

    6

    h-index

  3. Astronomy and Astrophysics

    6 publications · 395 citations

    6

    h-index

  4. The Astrophysical Journal

    ApJ · 4 publications · 412 citations

    4

    h-index

  5. Icarus

    2 publications · 31 citations

    2

    h-index

1–5