This thesis presents an analysis of CubeSat orbits for both Low Earth Orbit (LEO) and Sun-Synchronous Orbit (SSO) missions using Systems Tool Kit (STK). The study focuses on analyzing communication, power generation, and radiation exposure while considering various factors. The analysis is based on the 3U CubeSat called UT-ProSat-1, developed by students at Virginia Polytechnic Institute and State University (VT) for an upcoming mission. The orbit size and mass adjustments were made for the LEO mission to enhance communication performance. The influence of solar activity on CubeSat lifetime and access time was examined, highlighting the significance of mass and solar activity. The impact of increasing orbit size on communication time was analyzed, emphasizing the trade-offs between mass, orbit size, and communication performance. The SSO mission prioritized power generation optimization resulted in generating sufficient power for the nominal phase of the mission. It also considered the effects of the South Atlantic Anomaly (SAA) on radiation exposure. Effective risk management of increasing the shielding for the avionics were emphasized which consequently will stabilize the orbit and prolong its lifetime. Additionally, temperature dynamics were investigated, indicating the need for further analysis considering heat dissipation and utilizing a more accurate CubeSat model. The insights gained from this study contribute to the improved the performance of CubeSats and validate the mission results, providing valuable information for successful missions in the future. / Master of Science / This project explored the trajectories that small satellites, known as CubeSats, follow around Earth. Two main paths were investigated: the Low Earth Orbit (LEO), which is close to the Earth's surface, and the Sun Synchronized Orbit (SSO), which aligns with the Sun's movement. The software called Systems Tool Kit (STK) served as the simulation tool, helping to analyze the satellites' abilities to communicate, generate power, total space radiation, and satellite's temperature throughout the missions. The study was conducted on the satellite called UT-ProSat-1, a design by students from Virginia Polytechnic Institute and State University (VT). For the LEO path, changes to the satellite's size and weight were applied to analyze its effect on the communication capabilities. Also the Sun's effect on the satellite's operational life and communication windows was assessed. Changes in the satellite's orbit can influence its communication duration, and this necessitates a balance between its weight, trajectory, and communication capacity. Regarding the Sun-aligned path, SSO, the power generated from the Sun was sufficient for the satellite's power needs throughout its mission. A particular space zone with high radiation, the South Atlantic Anomaly (SAA), was evaluated. The majority of total radiation build up on the satellite was determined to came from this area. However, risks associated with this radiation can be minimized by enhancing protection for the satellite's electronics. Such measures not only safeguard the satellite but also increase its stability and longevity in space. The temperature behavior of the satellite was analyzed, underscoring the need for a deeper examination of its thermal patterns. Insights from this study will bolster CubeSat performance and provide valuable information for future successful space missions.

Currently, the Low Earth Orbit (LEO) space environment contains a growing number of orbital debris objects. This growing orbital debris population increases collision probabilities between both orbital debris and functioning satellites. A phenomenon known as Kessler Syndrome can be induced if these collisions occur. Kessler Syndrome states that these collisions can lead to an exponential increase in the orbital debris population, which could dangerously impede future space missions. Current literature outlines the necessity of stabilizing the near-Earth environment debris population and introduces the concept of active debris removal (ADR). The use of ADR on five orbital debris objects per year was found to be a requirement to achieve stability within the orbital debris population. A viable mission architecture is henceforth explored to utilize ADR for near-future execution to further develop research for orbital debris mitigation missions. The larger orbital debris objects are found in many different orbital regimes and are primarily composed of spent rocket bodies and retired satellites. Different orbital debris ranking schemes have been developed based on the population density in these different regimes, which are linked to higher collision probabilities. Using these ranking schemes, a set of target objects are selected to be investigated for this mission design that was composed of target objects with similar orbital characteristics that were not launched by the Commonwealth of Independent States (CIS) to minimize legal barriers. Different ADR capture and removal methods are inspected to find the optimal methods for this mission. An Analytical Hierarchy Process (AHP) has been used to assess these different methods, which utilizes comparisons of the different methods among a set of weighted criteria. A net capture method with a low thrust chemical engine for removal is identified as the optimal ADR method. The use of a laser detumbling system is also selected to stabilize target objects with a high rotation rate. A rendezvous and deorbit orbital analysis are conducted using both a low fidelity tool (for preliminary results) and a high fidelity tool (for more precise results). The rendezvous analysis is used to select a mission architecture that was composed of two different chaser satellites which rendezvous with the five different target objects by taking advantage of nodal precession. The deorbit analysis investigates different decay timelines and found the delta-v estimates that would be required to deorbit the target objects within the same year that they were captured in. These two orbital analyses provide valuable insight to the mission timeline, delta-v estimates, and approximate mass requirement for the chaser satellite and deorbit kits. The results of the target selection process, ADR selection process, and the rendezvous and deorbit analyses are meant to provide an initial concept and analysis for a near-future ADR mission. These approximate results provide insight and information to further develop orbital debris mitigation research to help solve the orbital debris population growth challenge for future space missions. / Master of Science / Currently, the near Earth space environment contains a growing number of space debris. This growth in the orbital debris population increases the likelihood of collisions with orbital debris, functioning satellites, and launch vehicles. These collisions can generate a chain of events that could exponentially increase the population of orbital debris, which at some scale could become a major obstacle for future space missions. Researchers have introduced the concept of active debris removal (ADR), which in simulations has been shown to help stabilize the growth of orbital debris. The use of ADR to remove as low as five orbital debris objects per year has been found to be sufficient to stabilize debris growth. A viable mission architecture using ADR technologies that can be implemented in the near future is henceforth explored to further develop research for orbital debris missions. The larger orbital debris objects are found in many different areas in space and are primarily made up of used rocket bodies and retired satellites. Different ranking schemes have been developed by researchers for these larger orbital debris objects based on the population density within these areas in space, which are linked to the chance of a collision. Using these ranking schemes, a set of orbital debris objects are selected to be targeted for this mission design. This set of selected target objects have similar orbital characteristics and the political/legal barriers that could be present during removal are minimal. An ADR mission is composed of two primary components, a capture method and a removal method, which are inspected to find the optimal methods for this mission. A decision-making technique, called an Analytical Hierarchy Process (AHP), has been used to assess these different methods. The AHP compares different capture and removal methods using a set of weighted criteria. A net capture method with small thrusters for removal is identified as the optimal ADR method. Additionally, the use of a laser system is selected to stabilize target objects that may be rotating too quickly for capture. An analysis on different mission architectures is conducted using both a low fidelity tool (for preliminary results) and a high fidelity tool (for more precise results). A mission architecture composed of two different "chaser" satellites which rendezvous with and deorbit the five different target objects is selected. The analysis used on the selected mission architecture provides valuable insight to the mission timeline, fuel estimates, and approximate mass requirements. The results of the target selection process, ADR selection process, and the mission architecture analysis are meant to provide an initial concept and introduce possible requirements for a nearfuture ADR mission. These approximate results provide information to further develop research that can help us solve the orbital debris population growth challenge for future space missions.

Staphylococcus aureus ist ein Kommensale, der die menschliche Haut und Schleimhaut der Nase und des Rachens besiedelt. Der Keim verursacht aufgrund zahlreicher Virulenzfaktoren leichte aber auch schwere Infektionen wie Pneumonie, Endokarditis oder Sepsis. Die Behandlung von S. aureus-Infektionen gestaltet sich heutzutage schwierig, da der Keim Resistenzen gegen verschiedenste Antibiotika ausgebildet hat. Zur Bekämpfung dieser Resistenzen werden neue Antibiotika benötigt, die u.a. mit der Zellphysiologie und der Zellwandwandsynthese der Bakterien interferieren. Die Zellphysiologie und Zellwandsynthese wird abhängig von der Wachstumsphase und Umwelt-einflüssen in den Bakterien streng reguliert. Neben den Zweikomponentensystemen sind Serin/Threonin-Proteinkinasen und -Phosphatasen wesentliche Sensoren und Regulatoren der Bakterien. Durch Phosphorylierung und Dephosphorylierung bewirken diese beiden Systeme eine Hemmung oder Aktivierung der entsprechenden Zielproteine. Dadurch kann sich die Bakterienzelle an innere und äußere Reize anpassen. In dieser Arbeit wurde die konservierte Serin/Threonin-Proteinkinase Stk und die Serin/Threonin-Phosphatase Stp von S. aureus untersucht. Die beiden Proteine Stk und Stp haben einen großen Einfluss auf die Signalweiterleitung, den zentralen Metabolismus, die Stressantwort, die Antibiotikaresistenz und die Virulenz von S. aureus. Im ersten Teil dieser Arbeit wird dargelegt, dass Stk und Stp in der bakteriellen Membran lokalisiert sind, dort miteinander interagieren und antagonistisch Zielproteine phosphorylieren bzw. dephospho-rylieren. Die Deletion der Phosphatase Stp bewirkt, dass zahlreiche Proteine in der Zelle permanent phosphoryliert und daher vermutlich nur noch eingeschränkt funktionstüchtig sind. Die ausbleibende Dephosphorylierung der Proteine in der stp-Mutante hat einen dramatischen Effekt auf die Zellwand-synthese und die Virulenz von S. aureus. So hat die stp-Mutante eine verdickte Zellwand und ist weniger virulent als die stk-Mutante und der Wildtypstamm. Im Rahmen dieser Arbeit wird erstmals eine Erklärung präsentiert, die die strukturellen Besonderheiten von Stk und deren Auswirkung auf die Zellwandsynthese zusammenführt: In der stp-Mutante akkumulieren Zellwandvorläufer in der Zelle, da vermutlich die entsprechenden Zellwandsyntheseproteine durch Stk-vermittelte Phosphorylierung gehemmt werden. Die Proteine FemXAB nehmen eine zentrale Rolle in der Zellwandsynthese ein, indem sie die Pentaglycin-Interpeptidbrücke des Zellwandvorläufers Pentaglycin-Lipid II syntheti-sieren. Stk wird durch die Bindung seiner extrazellulären Domänen an Pentaglycin-Lipid II aktiviert. In der vorliegenden Arbeit konnte FemX als in vitro Substrat von Stk und Stp identifiziert werden. Die permanente Phosphorylierung von FemX in der stp-Mutante führt zur verminderten Synthese der Pentaglycin-Brücken am Lipid II und infolgedessen zum Einbau von unvollständigen Muropeptiden in den neuen Peptidoglycanstrang. Diese strukturelle Veränderung führt zur Verdickung der Zellwand und folglich zur verminderten Empfindlichkeit gegenüber der Glycyl-Glycinpeptidase Lysostaphin. Neben FemX interagiert Stk mit weiteren Zellwandsyntheseproteinen wie FemAB und einigen Zellteilungsproteinen. Diese Ergebnisse verdeutlichen, dass Stk das Vorkommen seines extrazellulären Liganden Lipid II detektiert und dementsprechend die Zellwandsynthese über FemX reguliert. Im zweiten Teil der Arbeit wurde anhand verschiedener Omics-Techniken die stk-, stp- und stk/stp-Mutante im Vergleich zum S. aureus NewmanHG Wildtyp charakterisiert. Dabei zeigten sich teilweise große Unterschiede zwischen der stp-Mutante und den anderen Stämmen. Mit diesen Unter-suchungen konnten Ergebnisse aus anderen Studien bestätigt und mit weiteren Daten untermauert werden. So lässt sich die verminderte Virulenz der stp-Mutante mit der reduzierten Expression und Sekretion von Toxinen wie Hämolysinen und Leukozidinen erklären. Dies führt zu einer verminderten Hämolyse von Erythrozyten und einer verminderten Immunantwort gegen diese Toxine im Infektions-versuch. Stk und Stp phosphorylieren bzw. dephosphorylieren Transkriptionsfaktoren und Antwort-regulatoren von Zweikomponentensystemen, was zu der veränderten Expression und Sekretion der Virulenzfaktoren führt. Die Analyse der Mutanten offenbart, dass Stk ein negativer und Stp ein positiver Regulator der Virulenz in S. aureus ist. Außerdem regulieren Stk und Stp zentrale Aspekte des Metabolismus in S. aureus. So ist die Konzentration an Nukleotidtriphosphaten in der stp-Mutante reduziert, was auf eine verminderte Expression der Gene der Pyrimidinsynthese zurückzuführen ist. Anhand dieser Ergebnisse wird deutlich, dass Stk und Stp wesentliche Aspekte der Zellphysiologie wie die Zellwandsynthese, den zentralen Metabolismus und die Virulenz von S. aureus regulieren. / Staphylococcus aureus is a commensal that inhabits the human skin and mucosa. S. aureus causes a large variety of nosocomial and community-acquired infections. Nowadays, it is difficult to treat S. aureus infections because this bacterium has acquired resistance to multiple drugs. Therefore, there is a need for new antimicrobial drugs against S. aureus. The most promising strategy to combat antibiotic resistance is to find novel antibiotics which interfere with the cell physiology and cell wall synthesis pathway. The cell physiology and cell wall synthesis is tightly regulated depending on the bacterial growth phase and environmental influences. In addition to the two-component systems, serine/threonine protein kinases are essential sensors and regulators of bacteria. By phosphorylation and dephosphorylation, these systems cause inhibition or activation of the corresponding target proteins. This allows the bacterial cell to adapt to internal and external stimuli. In this work, the conserved serine/threonine protein kinase Stk and the phosphatase Stp in S. aureus were investigated. The two proteins Stk and Stp influence signal transduction, central metabolism, stress response, antibiotic resistance and virulence of S. aureus. In the first part of this work it is shown that Stk and Stp are localized in the bacterial membrane, where they interact with each other and phosphorylate or dephosphorylate target proteins antagonistically. The deletion of the phosphatase Stp leads to numerous proteins in the cell being permanently phosphorylated, which renders them partially unfunctional. The lack of protein dephosphorylation in the stp mutant has a dramatic effect on cell wall synthesis and virulence of S. aureus. Thus, the stp mutant has a thickened cell wall and is less virulent than the stk mutant and the wild-type strain. This work brings together the structural characteristics of Stk and their effect on cell wall synthesis for the first time. In the stp mutant, cell wall precursors accumulate in the cell, presumably because the corresponding cell wall synthesis proteins are inhibited by Stk-mediated phosphorylation. The proteins FemXAB play a key role in cell wall synthesis by synthesizing the pentaglycine interpeptide bridge of the final cell wall precursor pentaglycine lipid II. The pentaglycine lipid II is bound by the extracellular domains of Stk, thereby activating Stk. In the present work, FemX was identified as an in vitro substrate of Stk and Stp. The permanent phosphorylation of FemX in the stp mutant leads to inhibited synthesis of the pentaglycine bridges on the lipid II and consequently to the incorporation of incomplete muropeptides into the new peptidoglycan strand. This structural change leads to thickening of the cell wall and consequently reduced sensitivity to the glycyl-glycine peptidase lysostaphin. In addition to FemX, Stk interacts with other cell wall synthesis proteins such as FemAB and some cell division proteins. These results illustrate that Stk detects the presence of its extracellular ligand lipid II. This leads to an inhibition of FemX and a downregulation of the cell wall synthesis pathway. In the second part of this work, the stk, stp and stk/stp mutants were characterized by different omics- techniques in comparison to the S. aureus NewmanHG wild-type. There were some major differences between the stp mutant and the other strains. With these investigations, results from other studies were confirmed and substantiated with further data. Thus, the reduced virulence of the stp mutant can be explained by the reduced expression and secretion of toxins such as hemolysins and leukocidines. This leads to a reduced hemolysis of erythrocytes and a reduced immune response to these toxins in the infection experiment. Stk and Stp phosphorylate or dephosphorylate transcription factors and response regulators of two-component systems resulting in altered expression and secretion of virulence factors. Analysis of the mutants reveals that Stk is a negative and Stp is a positive regulator of virulence in S. aureus. In addition, Stk and Stp regulate central aspects of S. aureus metabolism. Thus, the concentration of nucleotide triphosphates in the stp mutant is reduced, which is due to a reduced expression of the genes of pyrimidine synthesis. From these results it becomes clear that Stk and Stp regulate essential aspects of cell physiology such as cell wall synthesis, central and virulence in S. aureus. This study of the function of Stk and Stp contributes significantly to the understanding of regulatory processes by phosphorylation in the bacterial cell.

This thesis deals with the evaluation of the technical condition of cars. Introduces legislative conditions for evaluation of technical condition of cars. Summarizes theoretical basis for possible failures of cars and their causes, sorted by individual functional groups. The practical part applies theoretical basis on the specific experiment and describes the principle of the methods utilized in the evaluation and compares it with the other methods, which can be also used for this operation.

We are in an era of massive spending cuts in educational institutions, aerospace companies and governmental entities. Educational institutions are pursuing more training for less money, aerospace companies are reducing the cost of gaining ight heritage and the government is cutting budgets and their response times. Organizations are accomplishing this improved efficiency by moving away from large-scale satellite projects and developing pico and nanosatellites following the CubeSat specifications. One of the major challenges of developing satellites to the standard CubeSat mission requirements is meeting the exceedingly tight power, data and communication constraints. A MATLAB toolbox was created to assist the CubeSat community with understanding these restrictions, optimizing their systems, increasing mission success and decreasing the time building to these initial requirements. The Toolbox incorporated the lessons learned from the past nine years of CubeSats' successes and Analytical Graphics, Inc. (AGI)'s Satellite Tool Kit (STK). The CubeSat Mission Planning Toolbox (CMPT) provides graphical representations of the important requirements a systems engineer needs to plan their mission. This includes requirements for data storage, ground station facilities, orbital parameters, and power. CMPT also allows for a comparison of broadcast (BC) downlinking to Ground Station Initiated (GSI) downlinking for payload data using federated ground station networks. Ultimately, this tool saves time and money for the CubeSat systems engineer

Renewed interest in returning to the Moon, emboldened by recent directives and missions by NASA, has necessitated the establishment of lunar infrastructure to support continuous human presence. With that, the objective of making this return more cost effective has gained significant importance. Low energy lunar transfers are more efficient ways to reach the Moon than the traditional Hohmann-type transfer. These trajectories leverage the multi-body gravitational effects to reduce overall delta-v requirements, in some cases removing the capture delta-v completely. While the time of flight for these transfers can be much longer than a Hohmann-type transfer, the chaotic design space of these transfers can enable large changes in arrival conditions at the Moon for small changes in initial conditions. Many investigations of these transfers take place in simplified dynamical models, such as the Planar Circular Restricted Three Body Problem, with very few higher-fidelity models being implemented. This approach is good to understand the dynamics of these trajectories as well as provide initial guesses for higher-fidelity models; but approximating the dynamics heavily make these models less applicable to mission design. This thesis aims to investigate the application of a higher-order model to simulate these trajectories. STK Astrogator was used to recreate the NASA GRAIL trajectory; and from the recreated trajectory, a nominal trajectory absent of mid-course corrections was established. This nominal trajectory was used to perform parametric and variational studies of departure and arrival conditions as well as compare to a nominal trajectory in a reduced-fidelity model. An investigation into the post launch correction burn requirements following launch vehicle under-performance was completed. Utilizing low energy transfers proved beneficial to adjusting arrival conditions for low delta-v requirements. All arrival inclinations are reasonably achievable for around 255 m/s. Using 255 m/s as a baseline, right ascension of the ascending node could be reached in a 40 degree range and argument of periapsis in a 50 degree range. Lunar insertion arrival can be varied by 7 hours on either side for less than 80 m/s. Trans-lunar injection epoch can be varied by 7 hours on either side of nominal departure for less than 4 m/s. Orbit radius and initial velocity are the most expensive errors to correct. These trajectories can be tuned to reduce the overall mid-course correction delta-v requirement for differing arrival inclinations if other orbital elements are relaxed. A relationship between placement of post-launch correction maneuver for velocity or radius errors was found. Comparing the trajectory in STK to the Inclined Bi-Elliptic Restricted Four Body problem, revealed that timing of the trajectory is variable while keeping the same arrival and departure conditions. However, solar radiation pressure cannot be ignored for more accurate simulation of these trajectories. This investigation has shown that low energy lunar transfers are a viable method to reach the Moon and their chaotic nature can be leveraged to relax restrictions in the design space. / Master of Science / Returning to the Moon has become a more important goal within the space industry. This has required more cost-efficient ways to reach the Moon; an important cost savings being fuel. Traditional ways to reach the Moon required large amounts of fuel to be expended to remain around the Moon after launch. Low energy lunar transfers aim to reduce fuel usage while still reaching the Moon, although they take much longer to reach their destination. Fuel and energy have direct comparisons and are used to evaluate these transfers. These transfers are highly susceptible to changes in their trajectory making them ideal for transferring to the Moon in different orientations. These changes can be made using very little fuel, allowing for more resources to be brought to the Moon. Navigating these transfers to the Moon require an accurate model of space for mission design.

Ce travail porte sur l’étude des mécanismes de phosphorylation des protéines par les sérine/thréonine kinases chez Staphylococcus aureus. Nous avons, tout d’abord, mis en évidence et caractérisé une seconde Ser/Thr-kinase, nommée Stk2. Cette kinase présente peu d’homologies avec les autres Ser/Thr-kinases bactériennes décrites à ce jour, en particulier avec la première Ser/Thr-kinase mise en évidence précédemment chez S. aureus, Stk1. Nous avons ensuite caractérisé dix sites d’autophosphorylation de Stk2 et nous avons montré que trois sites sont nécessaires à son activité. Enfin, nous avons montré que le régulateur global de virulence, SarA, est phosphorylé à la fois par Stk1 et Stk2. La phosphorylation de SarA influence sa capacité de liaison à l’ADN. Cette étude contribue à mieux appréhender, au niveau moléculaire, le rôle des Ser/Thr-kinases dans le métabolisme des bactéries et, plus particulièrement, dans la régulation de leur virulence / We report that protein phosphorylation on serine and threonine is required for controlling staphylococcal virulence. We identified and characterized a second serine/threonine kinase, Stk2, in S. aureus. Biochemical analyses revealed that this enzyme displays autokinase activity on both threonine and serine residues. Stk2 is atypical in the sense that it exhibits a weak similarity with the first Ser/Thr-kinase previously detected, Stk1, and its undergoes a different mechanism of activation compared to the other bacterial Ser/Thr-kinases described so far. We also showed that SarA, a major transcription factor that regulates more than a hundred virulence genes, is phosphorylated by both Stk1 and Stk2. Phosphorylation of SarA leads to strong effects on its ability to bind DNA. The study of Stk1 and Stk2, at the molecular level, provides a better understanding of the role of these staphylococcal Ser/Thr-kinases in bacterial metabolism and, in particular, in the regulation of virulence

The GPS data from Challenging Mini-satellite Payload (CHAMP) is used for its orbit determination for the epoch day of January 1st 2002.  The orbit of CHAMP is computed from the GPS data and ionospheric effects are removed by frequency combination. Further, the orbits of CHAMP for the same epoch day are computed using the satellite tool kit (STK) employing simplified general perturbations (SGP4) and a high precision orbit propagator (HPOP). Results from both techniques (GPS computed orbit and STK computed orbit) are compared. Furthermore, orbits computed using GPS data are also compared with jet propulsion laboratory’s published CHAMP spacecraft orbit and we have found that root mean square difference in ECEF position X component is below 0.01km other than some spikes at poles. The standard deviation of the difference in ECEF position X coordinate is 11.7m. The accuracy of our computed satellite positions (using GPS data) is about 12 metres for other than polar areas. However there are some occasional spikes, especially at poles, having maximum errors (about 0.055 km).

GPS data from Challenging Mini-satellite Payload (CHAMP) is used for its orbit determination for the epoch day of January 1st 2002.  The orbit of CHAMP is computed from the GPS data and ionospheric effects are removed by frequency combination. Further, the orbits of CHAMP for the same epoch day are computed using the satellite tool kit (STK) employing simplified general perturbations (SGP4) and a high precision orbit propagator (HPOP). Furthermore, orbits computed using GPS data are also compared with jet propulsion laboratory’s published CHAMP spacecraft orbit and we have found that root mean square difference in ECEF position X component is below 0.01km other than some spikes at poles. The standard deviation of the difference in ECEF position X coordinate (JPL results – GPS computed results) is 11.7m. Since JPL computed orbits are considered as true orbits of CHAMP with accuracy of centimeter level (https://gipsy-oasis.jpl.nasa.gov/). Therefore this difference can also be referred as observed error in GPS computed orbits. Considering above discussion, we can expect that accuracy of our computed satellite positions (using GPS data) is about 12 metres for other than poles area. However there are some occasional spikes, especially at poles, having maximum errors (about 0.055 km).

Eccentric lunar frozen orbits are analyzed in this study in relation to lunar navigation and communications missions, particularly the proposed Magnolia-1 mission. An overview of the Earth/Moon system, frozen orbits, and the Magnolia-1 mission is provided. A review of existing literature is presented, and potential limitations are discussed. Both preliminary and numerical perturbation analyses are presented, and a general set of perturbations for further analysis of high-altitude lunar orbits is identified. Analysis of potential orbits for the Magnolia-1 mission is performed through calculation of a maximum deviation metric and through visualization as a function of initial orbital elements. Trends are identified within a closed search space by varying elements individually and in combination. Potential orbit designs for the Magnolia-1 mission are selected and compared to established alternatives. A method of orbit refinement is used to improve behavior, and coverage and eclipse analyses are performed to establish suitability. Conclusions are made involving general trends related to eccentric lunar frozen orbits and the specific designs proposed for the Magnolia-1 mission, and a method for the design of similar orbits is suggested. Ideas for further study are also presented.