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
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4.9K
Citations
255
Authors
114
Institutions
Publications per year
2017–2026
14
Variants
Heo
Parents
62
Outward radial diffusion driven by losses at magnetopause
Yuri Shprits, R. M. Thorne, R. Friedel et al. · Journal of Geophysical Research Atmospheres · 2006 · 378 citations · Full text
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114
Goddard Space Flight Center
Greenbelt, United States
6 h-index
8 publications
95 citations
California Institute of Technology
Pasadena, United States
5 h-index
15 publications
634 citations
The Aerospace Corporation
El Segundo, United States
4 h-index
6 publications
581 citations
Environment and Climate Change Canada
Ottawa, Canada
4 h-index
8 publications
145 citations
University of Colorado Boulder
Boulder, United States
4 h-index
7 publications
1.3K citations
Natural Resources Canada
Ottawa, Canada
4 h-index
8 publications
145 citations
Politecnico di Milano
Milan, Italy
3 h-index
3 publications
62 citations
a.i. solutions (United States)
Lanham-Seabrook, United States
3 h-index
4 publications
46 citations
1–8 of 114
ApJ · 8 publications · 2.5K citations
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4 publications · 173 citations
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3 publications · 164 citations
3
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3 publications · 124 citations
3
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JGR · 3 publications · 563 citations
3
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