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What are ground tracks?
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COE Determination
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a e i ? ? ? ? ? ? COE Determination
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Non-rotating Earth
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Rotating Earth
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COE Determination Semimajor axis Δ longitude ΔNΔN P = ΔN 15º / hr
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a e i ? ? ? ? COE Determination ?
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Eccentricity Circle
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COE Determination Eccentricity
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COE Determination Eccentricity Line Symmetry Ellipse
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COE Determination Eccentricity Line Symmetry Ellipse
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COE Determination Eccentricity Line Symmetry Ellipse
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COE Determination Eccentricity Line Symmetry Ellipse
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COE Determination Eccentricity Line Symmetry Ellipse
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COE Determination Eccentricity Line Symmetry Ellipse
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COE Determination Eccentricity Line Symmetry Ellipse
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COE Determination Eccentricity
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COE Determination Eccentricity Hinge Symmetry Ellipse
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COE Determination Hinge Symmetry Eccentricity Ellipse
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COE Determination Hinge Symmetry Eccentricity Ellipse
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COE Determination Hinge Symmetry Eccentricity Ellipse
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COE Determination Hinge Symmetry Eccentricity Ellipse
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COE Determination Eccentricity Hinge Symmetry Ellipse
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COE Determination Eccentricity
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COE Determination Eccentricity Line & Hinge Circle
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COE Determination Eccentricity Neither Ellipse
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COE Determination Eccentricity
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a e i ? ? ? ? COE Determination ~
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Inclination i = highest latitude
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COE Determination Inclination i = 180º - highest latitude
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COE Determination Inclination i = highest latitude
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COE Determination Inclination i = 180º - highest latitude
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a e i ? ? ? COE Determination ~
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a e i ? ? COE Determination ~
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Argument of Perigee
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COE Determination 360º per orbit 90º 180º 270º 360º Ascending Node Argument of Perigee
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Perigee = 180 Perigee = 270 Perigee = 90 Perigee = 0 Hinge Symmetric Line Symmetric
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COE Determination Argument of Perigee ω = 180º
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COE Determination Argument of Perigee ω = 90º
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COE Determination Argument of Perigee ω = 0º
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COE Determination Argument of Perigee ω = 270º
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COE Determination Argument of Perigee Hinge Symmetry ω = 0º or 180º
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COE Determination Argument of Perigee Line Symmetry ω = 90º or 270º
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a e i ? COE Determination ~ ~
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True Anomaly
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COE Determination True Anomaly
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COE Determination True Anomaly
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Orbit Examples
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Molniya
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Geostationary
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Geosynchronous
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e = 0.8 = 180 e = 0.8 = 0 e = 0.0
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Geosynchronous e = 0 i = 0 e = 0.4 = 180 e = 0.6 = 90
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