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1

Wiesel, William E. Modern orbit determination. Aphelion Press, 2003.

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2

Burns, Rowland E. Forbidden tangential orbit transfers between intersecting Keplerian orbits. National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division, 1990.

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3

Buglia, James J. Direct computation of orbital sunrise or sunset event parameters. National Aeronautics and Space Administration, Scientific and Technical Information Branch, 1986.

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4

Kyo, Nishiyama, ed. Nilpotent orbits, associated cycles, and Whittaker models for highest weight representations. Société Mathématique de France, 2001.

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5

Mission geometry: Orbit and constellation design and management : spacecraft orbit and attitude systems. Microcosm Press, 2001.

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6

Wertz, James Richard. Mission geometry: Orbit and constellation design and management : spacecraft orbit and attitude systems. Microcosm Press, 2001.

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7

M, Ware George, MacConochie Ian O, and Langley Research Center, eds. Subsonic aerodynamic characteristics of a circular body earth-to-orbit vehicle. National Aeronautics and Space Administration, Langley Research Center, 1996.

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8

Meeting, COSPAR Plenary. Orbit determination and analysis: Proceedings of the PSD Meeting of the COSPAR Technical Panel on Satellite Dynamics which was held during the Thirtieth COSPAR Scientific Assembly, Hamburg, Germany, 11-21 July 1994. Published for The Committee on Space Research [by] Pergamon, 1995.

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9

Stanley, Turner Michael, Fermi National Accelerator Laboratory, and United States. National Aeronautics and Space Administration., eds. Second-order reconstruction of the inflationary potential. Fermi National Accelerator Laboratory, 1994.

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10

Stanley, Turner Michael, Fermi National Accelerator Laboratory, and United States. National Aeronautics and Space Administration., eds. Second-order reconstruction of the inflationary potential. Fermi National Accelerator Laboratory, 1994.

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11

Stanley, Turner Michael, Fermi National Accelerator Laboratory, and United States. National Aeronautics and Space Administration., eds. Second-order reconstruction of the inflationary potential. Fermi National Accelerator Laboratory, 1994.

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12

1961-, Eberhard Gill, ed. Satellite orbits: Models, methods, and applications. Springer, 2000.

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13

Montenbruck, Oliver. Satellite orbits: Models, methods, and applications. Springer, 2000.

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14

Jet Propulsion Laboratory (U.S.), ed. Cosmic ray environment model for earth orbit: Final report. National Aeronautics and Space Administration, Jet Propulsion Laboratory, California Institute of Technology, 1985.

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15

Černoušková, Dagmar. Orbis pictus Bohuslava Fuchse: Orbis pictus von Bohuslav Fuchs = Orbis pictus de Bohuslav Fuchs = Orbis pictus of Bohuslav Fuchs. Muzeum města Brna, 2012.

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16

Luthcke, S. B. Nonconservative force model parameter estimation strategy for TOPEX/Poseidon precision orbit determination. National Aeronautics and Space Administration, Goddard Space Flight Center, 1992.

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17

Reilly, Charles H. A satellite system synthesis model for orbital arc allotment optimization. National Aeronautics and Space Administration, Lewis Research Center, 1987.

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18

King-Hele, D. G. Satellite orbits in an atmosphere: Theory and applications. Blackie, 1987.

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19

C, Foster Stephen, ed. The eastern Dada orbit: Russia, Georgia, Ukraine, Central Europe and Japan. G.K. Hall, 1996.

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20

United States. National Aeronautics and Space Administration. Scientific and Technical Information Program., ed. High degree gravitational sensitivity from Mars orbiters for the GMM-1 gravity model. National Aeronautics and Space Administration, Scientific and Technical Information Program, 1993.

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21

Jehn, Rüdiger. Modelling debris clouds. Shaker Verlag, 1996.

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22

J, Kessler Donald, and United States. National Aeronautics and Space Administration., eds. A computer-based orbital debris environment model for spacecraft design and observation in low earth orbit. National Aeronautics and Space Administration, 1996.

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23

J, Kessler Donald, and United States. National Aeronautics and Space Administration., eds. A computer-based orbital debris environment model for spacecraft design and observation in low earth orbit. National Aeronautics and Space Administration, 1996.

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24

J, Kessler Donald, and United States. National Aeronautics and Space Administration., eds. A computer-based orbital debris environment model for spacecraft design and observation in low earth orbit. National Aeronautics and Space Administration, 1996.

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25

J, Kessler Donald, and United States. National Aeronautics and Space Administration., eds. A computer-based orbital debris environment model for spacecraft design and observation in low earth orbit. National Aeronautics and Space Administration, 1996.

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26

Jean-Pierre, Carrou, and Centre spatial de Toulouse, eds. Mécanique spatiale. Cépaduès-Editions, 1995.

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27

Tomlinson, Barbara S. Use of random Martian atmosphere to evaluate potential entry guidance schemes. National Aeronautics and Space Administration, Langley Research Center, 1990.

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28

Görlach, Thomas. Semi-analytische Langzeitvorausberechnung von hohen Satellitenbahnen als Basis für die Bahnsteuerung. Shaker, 1996.

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29

1979-, Wang Jiongqi, Pan Xiaogang 1979-, and Jiao Yuanyuan 1982-, eds. Wei xing zhuang tai rong he gu ji li lun yu fang fa. Ke xue chu ban she, 2013.

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30

David, Chadwell C., and United States. National Aeronautics and Space Administration., eds. Investigation for improving Global Positioning System (GPS) orbits using a discrete sequential estimator and stochastic models of selected physical processes. Ohio State University, 1993.

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31

L, Colborn B., and United States. National Aeronautics and Space Administration., eds. LDEF satellite radiation analyses: Final report, contract no. NAS8-39386. Science Applications International Corp., 1996.

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32

L, Colborn B., and United States. National Aeronautics and Space Administration., eds. LDEF satellite radiation analyses: Final report, contract no. NAS8-39386. Science Applications International Corp., 1996.

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33

Vondrak, R. R. Lunar reconnaissance orbiter mission. Springer, 2010.

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34

Center, Goddard Space Flight, ed. AEOSS design guide for system analysis on Advanced Earth-Orbital Spacecraft Systems. National Aeronautics and Space Administration, Goddard Space Flight Center, 1990.

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35

Center, Goddard Space Flight, ed. AEOSS design guide for system analysis on Advanced Earth-Orbital Spacecraft Systems. National Aeronautics and Space Administration, Goddard Space Flight Center, 1990.

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36

Milani, Andrea. Non-gravitational perturbations and satellite geodesy. A. Hilger, 1987.

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37

Center, Goddard Space Flight, ed. AEOSS runtime manual for system analysis on Advanced Earth-Orbital Spacecraft Systems. National Aeronautics and Space Administration, Goddard Space Flight Center, 1990.

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38

Labacensium, Academia Operosorum. Apes academicae operosorum Labacensium, sive, Institutum, leges, scopus, nomina, et symbola novae academiae sub apum symbolo Labaci adunatae, orbi literario exhibitae cum oratione inaugurali in primo conventu publico ad proceres Aemonae dicta. Slovenska akademija znanosti in umetnosti, 1988.

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39

Proles vaesana Philippi totius malleus orbis: Die Alexandreis des Walter von Chatillon und ihre Neudeutung von Lucans Pharsalia im Sinne des typologischen Geschichtsverständnisses. Saur, 2001.

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40

Tapley, Byron, Bob Schutz, and George H. Born. Statistical Orbit Determination. Elsevier Science & Technology Books, 2004.

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41

Tapley, Byron, Bob Schutz, and George H. Born. Statistical Orbit Determination. Academic Press, 2004.

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42

Statistical Orbit Determination. Academic Press, 2004.

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43

Modern Orbit Determination: Second Edition. CreateSpace Independent Publishing Platform, 2010.

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44

On-Orbit Operations Optimization: Modeling and Algorithms. Springer New York, 2014.

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45

Cao, Gang, and Lance DeLong. Physics of Spin-Orbit-Coupled Oxides. Oxford University Press, 2021. http://dx.doi.org/10.1093/oso/9780199602025.001.0001.

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Prior to 2010, most research on the physics and chemistry of transition metal oxides was dominated by compounds of the 3d-transition elements such as Cr, Mn, Fe, Co, Ni, and Cu. These materials exhibited novel, important phenomena that include giant magnetoresistance in manganites, as well as high-temperature superconductivity in doped La<sub>2</sub>CuO<sub>4</sub> and related cuprates. The discovery in 1994 of an exotic superconducting state in Sr<sub>2</sub>RuO<sub>4</sub> shifted some interest toward ruthenates. Moreover, the realization in 2008 that a novel variant of the classic Mott meta
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46

National Aeronautics and Space Administration (NASA) Staff. Determination of the Orbit of the Japanese Satellite Ajisai and the Gem-T1 and Gem-T2 Gravity Field Models. Independently Published, 2018.

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47

Wittman, David M. Orbits. Oxford University Press, 2018. http://dx.doi.org/10.1093/oso/9780199658633.003.0017.

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Orbits are ubiquitous in the universe: moons orbit planets, planets orbit stars, stars orbit around the center of the Milky Way galaxy, and so on. Any theory of gravity will have to explain the properties of all these orbits. To pave the way for developing the metric theory of gravity (general relativity) this chapter examines the basics of orbits as observed and as explained by the Newtonian model of gravity. We can use our understanding of gravity to infer the masses and other properties of these cosmic systems. Te chapter concludes with four optional sections in this spirit, covering the sl
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48

Gill, Eberhard, and Oliver Montenbruck. Satellite Orbits: Models, Methods and Applications. Springer, 2005.

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49

Gill, Eberhard, and Oliver Montenbruck. Satellite Orbits: Models, Methods and Applications. Springer Berlin / Heidelberg, 2013.

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50

Gill, Eberhard, and Oliver Montenbruck. Satellite Orbits: Models, Methods and Applications. Springer, 2012.

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