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. 2023 Oct 19;219(8):65. doi: 10.1007/s11214-023-01013-6

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© The Author(s) 2023

Open Access This article is licensed under a Creative Commons Attribution 4.0 International License, which permits use, sharing, adaptation, distribution and reproduction in any medium or format, as long as you give appropriate credit to the original author(s) and the source, provide a link to the Creative Commons licence, and indicate if changes were made. The images or other third party material in this article are included in the article’s Creative Commons licence, unless indicated otherwise in a credit line to the material. If material is not included in the article’s Creative Commons licence and your intended use is not permitted by statutory regulation or exceeds the permitted use, you will need to obtain permission directly from the copyright holder. To view a copy of this licence, visit http://creativecommons.org/licenses/by/4.0/.

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Fig. 4 — The PERSEUS orbit is high-inclination relative to the planet’s poles, but remains low-inclination relative to the ecliptic plane. PERSUES’s apoapsis is in the dawn dayside sector and precesses slightly towards to the Sun-Uranus line (as viewed from ecliptic north) over the two-year baseline mission. This simulation shows the PERSUES orbit (green) relative to an idealistic magnetopause (gray mesh surface) based on the Voyager 2 observations, the orbits of several inner moons (blue), and several radial distances and MLTs of dipolar magnetic field lines (dashed pink)