Research Article
Multisegment Scheme Applications to Modified Chebyshev Picard Iteration Method for Highly Elliptical Orbits
Table 1
Classical orbital elements.
| Parameter | Symbol | Value | Unit |
| Semimajor axis | | | m | Eccentricity | | 0.7 | ā | Inclination | | 60 | Degree | Right ascension of the ascending node | | 45 | Degree | Argument of periapsis | | 30 | Degree | Orbit period | | | s |
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