Highly Elliptical Orbits

Highly Elliptical Orbits is a type of satellite orbit characterized by a high orbital eccentricity, typically with values exceeding 0.5, resulting in a significant difference between perigee and apogee altitudes, thereby enabling prolonged dwell times over high-latitude regions during the apogee phase.

62

Publications

4.9K

Citations

255

Authors

114

Institutions

Publications per year

2017–2026

14

Variants

Heo

Authors

255

  1. AP
    Alexander P. Trishchenko

    Natural Resources Canada, Canada

    4 publications · 79 citations

    4

    h-index

  2. LG
    Louis Garand

    Environment and Climate Change Canada, Canada

    4 publications · 79 citations

    4

    h-index

  3. CC
    Camilla Colombo

    Politecnico di Milano, Italy

    3 publications · 62 citations

    3

    h-index

  4. LT
    L. Trichtchenko

    Natural Resources Canada, Canada

    3 publications · 69 citations

    3

    h-index

  5. GD
    G. D. Reeves

    Los Alamos National Laboratory, United States

    3 publications · 576 citations

    3

    h-index

1–5 of 255

Venues

  1. The Astrophysical Journal

    ApJ · 8 publications · 2.5K citations

    8

    h-index

  2. Advances in Space Research

    4 publications · 173 citations

    4

    h-index

  3. Space Weather

    3 publications · 164 citations

    3

    h-index

  4. Journal of Guidance Control and Dynamics

    3 publications · 124 citations

    3

    h-index

  5. Journal of Geophysical Research Atmospheres

    JGR · 3 publications · 563 citations

    3

    h-index

1–5