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Abstract:Satellite coverage analysis commonly relies on intensive numerical computations to evaluate access and revisit times, resulting in high computational costs, particularly in long-term performance assessment and large-scale constellation analysis involving numerous satellites. To address this issue, this paper presents a semi-analytic method for rapid coverage analysis for a satellite using piecewise ellipse models. We introduce the epoch longitude of the ascending node (ELAN), defined as the longitude of the ascending node at the beginning of each nodal period. Since the shape of the ground track over one nodal period remains invariant, target visibility within the period is uniquely determined by ELAN. By identifying the feasible range of ELAN, the proposed method excludes invisible nodal periods, thereby substantially reducing search space. Within the feasible range, we transform the visibility-boundary relationship into a modified ELAN (MELAN) and approximate it using analytically invertible piecewise ellipse models, enabling direct evaluation of the entry and exit times without repeated time-domain visibility searches. By exploiting the periodic evolution of ELAN, the proposed method efficiently computes access and revisit times over a given time horizon. Numerical case studies over a wide range of orbital configurations and target latitudes show that the proposed method achieves sub-0.1% error in most cases while significantly reducing computational effort.

Submission history

From: Byeong-Un Jo [view email]
[v1] Sun, 31 May 2026 08:41:28 UTC (766 KB)