Perturbed Orbital Elements is a set of time-varying parameters that describe the instantaneous shape, size, and orientation of a satellite's orbit under the influence of non-Keplerian forces, distinguishing it from the constant elements of an ideal two-body system by accounting for gravitational, atmospheric, and other external perturbations.
173
Publications
7.6K
Citations
397
Authors
206
Institutions
Publications per year
2017–2026
30
Parents
Publications
173
The motion of a close earth satellite
Yoshihide Kozai · The Astronomical Journal · 1959 · 502 citations
Gordon J. F. MacDonald · Reviews of Geophysics · 1964 · 364 citations
1–5 of 173
Authors
397
- DJ
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1–5 of 397
Institutions
206
National Astronomical Observatory of Japan
Mitaka-shi, Japan
7 h-index
8 publications
203 citations
Eötvös Loránd University
Budapest, Hungary
6 h-index
7 publications
218 citations
University of Colorado Boulder
Boulder, United States
5 h-index
9 publications
338 citations
Sorbonne Université
Paris, France
5 h-index
17 publications
883 citations
Centre National de la Recherche Scientifique
Paris, France
5 h-index
26 publications
1.3K citations
Jet Propulsion Laboratory
Pasadena, United States
5 h-index
11 publications
274 citations
Adam Mickiewicz University in Poznań
Poznan, Poland
4 h-index
4 publications
127 citations
Konkoly Observatory
Budapest, Hungary
4 h-index
8 publications
417 citations
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Venues
- Journal of Guidance Control and Dynamics
23 publications · 715 citations
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- The Astronomical Journal
AJ · 18 publications · 1.4K citations
17
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- The Astrophysical Journal
ApJ · 14 publications · 494 citations
14
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- Monthly Notices of the Royal Astronomical Society
16 publications · 558 citations
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- Astronomy and Astrophysics
9 publications · 262 citations
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