What question did this study set out to answer?

The aim is to explore a novel navigation strategy for low Earth orbit satellites using the cosmic microwave background.

February 9, 20260 citationsOpen Access

The Law of Spatial Repulsion and Satellite Orbit Correction: The CMB Spatial Gradient Navigation Strategy

Key Points

The aim is to explore a novel navigation strategy for low Earth orbit satellites using the cosmic microwave background.
Proposing the Law of Spatial Repulsion based on CMB anisotropy.
Utilizing a position-dependent scalar field model to derive a navigation algorithm.
Simulating satellite thruster adjustments to align with local CMB temperature fluctuations.
Simulations indicate a potential reduction in propellant consumption by over 30%.
The proposed strategy could significantly extend satellite operational lifespan.

Abstract

Update v2. 0: CMB Spatial Gradient Navigation Strategy English Abstract This document outlines the Law of Spatial Repulsion (n=3. 42590) and its application in Low Earth Orbit (LEO) satellite navigation. By interpreting the Cosmic Microwave Background (CMB) anisotropy as a static Spatial Repulsion Map, this hypothesis proposes a "Resonance Surfing" strategy. Korean Abstract (국문 초록) 본 문서는 저궤도 (LEO) 위성 항법에 적용되는 **공간 척력 법칙 (n=3. 42590) **을 기술합니다. 우주 배경 복사 (CMB) 의 비등방성을 정적인 **'공간 척력 지도 (Spatial Repulsion Map) '**로 해석함으로써, 본 가설은 "공명 서핑 (Resonance Surfing) " 전략을 제안합니다. Key Formula (Spatial Gradient Navigation / 공간 기울기 항법 공식) Instead of high-frequency temporal pulsing, this model utilizes the position-dependent scalar field of the CMB. The corrected repulsive force F₍₄ₓ at position r is given by: F₍₄ₓ (r) = L^{3. 42590} 1 + (T (r) T₀ₕ₆) r: Satellite's current orbital position (위성의 현재 궤도 위치). T (r): Local CMB temperature fluctuation (국소 CMB 온도 편차).: Coupling constant determined by the satellite's propulsion responsiveness (결합 계수). Simulation Results: Simulations suggest that synchronizing thruster duty cycles with local CMB repulsive gradients can reduce propellant consumption by over 30%, significantly extending satellite operational lifespan. Licensing & Legal Notice / 라이선스 및 법적 고지 1. Copyright Ownership (저작권 소유) English: Copyright © 2026 Nam-ho Kim. All rights reserved. The intellectual property rights for the "Law of Spatial Repulsion, " the specific constant (n=3. 42590), and the "CMB Spatial Gradient Navigation Algorithm" reside solely with the author, Nam-ho Kim. Korean: 본 저작물, "공간 척력 법칙", 특정 상수 (n=3. 42590) 및 "CMB 공간 기울기 항법 알고리즘"에 대한 모든 지적 재산권은 저작자 김남호에게 있습니다. 2. Commercial Use (영리 목적 사용) English: STRICTLY PROHIBITED. Use of this theory, formula, or algorithm for commercial purposes (including but not limited to satellite manufacturing, orbit correction software, and telecommunications) is forbidden without a formal license agreement. Korean: 엄격히 금지 본 이론, 공식, 알고리즘을 영리 목적 (위성 제조, 궤도 보정 소프트웨어, 통신 산업 등) 으로 사용하는 것은 정식 라이선스 계약 없이는 불법입니다. 3. Military & Defense Applications (군사 및 국방 적용) English: RESTRICTED. Application in missile defense systems, ICBM trajectory calculation, or any weaponized spatial technology requires explicit written consent from the rights holder. Korean: 제한됨 미사일 방어 체계, ICBM 궤도 계산, 또는 무기화된 공간 기술에의 적용은 권리 보유자의 명시적인 서면 동의가 필요합니다. 4. Academic Use (학술적 이용) This work is licensed under a Creative Commons Attribution-NonCommercial-NoDerivatives 4. 0 International License (CC BY-NC-ND 4. 0).

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