CINXE.COM

<!DOCTYPE html PUBLIC "-//WAPFORUM//DTD XHTML Mobile 1.0//EN" "http://www.wapforum.org/DTD/xhtml-mobile10.dtd"><html xmlns="http://www.w3.org/1999/xhtml" lang="en-SG"><head><meta content="application/xhtml+xml; charset=UTF-8" http-equiv="Content-Type"/><meta content="no-cache" name="Cache-Control"/><title>argument of latitude - Google Search</title><style>a{text-decoration:none;color:inherit}a:hover{text-decoration:underline}a img{border:0}body{font-family:sans-serif;padding:8px;margin:0 auto;max-width:700px;min-width:240px;}.FbhRzb{border-left:thin solid #dadce0;border-right:thin solid #dadce0;border-top:thin solid #dadce0;height:40px;overflow:hidden}.n692Zd{margin-bottom:10px}.cvifge{height:40px;border-spacing:0}.QvGUP{height:40px;padding:0 8px 0 8px;vertical-align:top}.O4cRJf{height:40px;width:100%;padding:0;padding-right:16px}.O1ePr{height:40px;padding:0;vertical-align:top}.kgJEQe{height:36px;width:98px;vertical-align:top;margin-top:4px}.lXLRf{vertical-align:top}.MhzMZd{border:0;vertical-align:middle;font-size:14px;height:40px;padding:0;width:100%;padding-left:16px}.xB0fq{height:40px;border:none;font-size:14px;background-color:#1a73e8;color:#fff;padding:0 16px;margin:0;vertical-align:top;cursor:pointer}.xB0fq:focus{border:1px solid #1a73e8}.M7pB2{border:thin solid #dadce0;margin:0 0 3px 0;font-size:13px;font-weight:500;height:40px}.euZec{width:100%;height:40px;text-align:center;border-spacing:0}table.euZec td{padding:0;width:25%}.QIqI7{display:inline-block;padding-top:4px;font-weight:bold;color:#4285f4}.EY24We{border-bottom:2px solid #4285f4}.CsQyDc{display:inline-block;color:#70757a}.TuS8Ad{font-size:14px}.HddGcc{padding:8px;color:#70757a}.dzp8ae{font-weight:bold;color:#3c4043}.rEM8G{color:#70757a}.bookcf{table-layout:fixed;width:100%;border-spacing:0}.InWNIe{text-align:center}.uZgmoc{border:thin solid #dadce0;color:#70757a;font-size:14px;text-align:center;table-layout:fixed;width:100%}.frGj1b{display:block;padding:12px 0 12px 0;width:100%}.BnJWBc{text-align:center;padding:6px 0 13px 0;height:35px}</style></head><body><style>.ezO2md{border:thin solid #dadce0;padding:12px 16px 12px 16px;margin-bottom:10px;font-family:sans-serif}.lIMUZd{font-family:sans-serif}.synv3b{padding-bottom:12px}.FYYwXe{padding-bottom:12px}.oO6lG{padding-top:12px}.LUX65{overflow:hidden;text-align:center}.DT7Nxc{margin:0 auto;display:block}.HeLCGb{margin:0 -50%;display:inline-block}.CSfvHb{padding-bottom:8px}.fYyStc{word-break:break-word}.ynsChf{display:block;white-space:nowrap;overflow:hidden;text-overflow:ellipsis}.Fj3V3b{color:#1967d2;font-size:14px;line-height:20px}.FrIlee{color:#202124;font-size:13px;line-height:20px}.F9iS2e{color:#70757a;font-size:13px;line-height:20px}.WMQ2Le{color:#70757a;font-size:12px;line-height:16px}.x3G5ab{color:#202124;font-size:18px;line-height:24px}.fuLhoc{color:#1967d2;font-size:18px;line-height:24px}.epoveb{font-size:32px;line-height:40px;font-weight:400;color:#202124}.dXDvrc{color:#0d652d;font-size:14px;line-height:20px;word-wrap:break-word}.dloBPe{font-weight:bold}.YVIcad{color:#70757a}.JkVVdd{color:#ea4335}.oXZRFd{color:#ea4335}.MQHtg{color:#fbbc04}.pyMRrb{color:#1e8e3e}.EtTZid{color:#1e8e3e}.M3vVJe{color:#1967d2}.qXLe6d{display:block}.NHQNef{font-style:italic}.Cb8Z7c{white-space:pre}a.ZWRArf{text-decoration:none}a .CVA68e:hover{text-decoration:underline}.Dks9wf{width:100%}.KZhhub{border-spacing:0;width:100%}.udTCfd{vertical-align:top;width:100%}.GN4D8d{margin:0}.ZuwI5d{border-spacing:0;width:100%}.qPa7sb{display:block;float:right;padding-left:16px}.AS66f{padding-top:12px}.SqPqqd{display:block;padding-top:12px}.VeHcBf{border-spacing:0;width:100%;table-layout:auto;padding:4px 0 4px 0}.MGsU1d{text-align:right}</style><div class="n692Zd"><div class="BnJWBc"><a class="lXLRf" href="/?sca_esv=bbb4249b07bbd0d1&output=search&sa=X&ved=0ahUKEwih4sDR_cuLAxW7SWwGHTUGAvcQPAgC"><img class="kgJEQe" src="/images/branding/searchlogo/1x/googlelogo_desk_heirloom_color_150x55dp.gif" alt="Google"/></a></div><div class="FbhRzb"><form action="/search"><input name="sca_esv" value="bbb4249b07bbd0d1" type="hidden"/><input name="oq" type="hidden"/><input name="aqs" type="hidden"/><table class="cvifge"><tr><td class="O4cRJf"><input class="MhzMZd" value="argument of latitude" name="q" type="text"/></td><td class="O1ePr"><input class="xB0fq" value="Search" type="submit"/></td></tr></table></form></div><div class="M7pB2"><table class="euZec"><tbody><tr><td class="EY24We"><span class="QIqI7">ALL</span></td><td><a class="CsQyDc" href="/search?q=argument+of+latitude&sca_esv=bbb4249b07bbd0d1&tbm=isch&source=lnms&sa=X&ved=0ahUKEwih4sDR_cuLAxW7SWwGHTUGAvcQ_AUIBSgB">IMAGES</a></td><td><a class="CsQyDc" href="/search?q=argument+of+latitude&sca_esv=bbb4249b07bbd0d1&tbm=vid&source=lnms&sa=X&ved=0ahUKEwih4sDR_cuLAxW7SWwGHTUGAvcQ_AUIBigC">VIDEOS</a></td><td><a class="CsQyDc" href="/search?q=argument+of+latitude&sca_esv=bbb4249b07bbd0d1&tbm=nws&source=lnms&sa=X&ved=0ahUKEwih4sDR_cuLAxW7SWwGHTUGAvcQ_AUIBygD">NEWS</a></td></tr></tbody></table></div></div><div><div> <div> <div class="ezO2md"><div><div class="FYYwXe"> <div> <span class="qXLe6d FrIlee"> <span class="fYyStc">u: Argument of latitude is </span> <span class="dloBPe fYyStc">the sum of argument of perigee and true anomaly</span> <span class="fYyStc">. It is the angle measured from the equator to the satellite at a particular epoch. For the circular orbits the argument of perigee is not well defined, therefore it is more convenient to use the argument of latitude instead.</span> </span> </div> </div><div><a class="fuLhoc ZWRArf" href="/url?q=https://www.gsc-europa.eu/system-service-status/orbital-and-technical-parameters&sa=U&ved=2ahUKEwih4sDR_cuLAxW7SWwGHTUGAvcQFnoECAIQAg&usg=AOvVaw31fwDV1-wJhkXfsRxAWQjx"><span class="CVA68e qXLe6d">Orbital and Technical Parameters | European GNSS Service Centre ...</span> <span class="qXLe6d dXDvrc"> <span class="fYyStc">www.gsc-europa.eu › system-service-status › orbital-and-technical-paramet...</span> </span> </a></div><div class="oO6lG"> <span class="qXLe6d F9iS2e WMQ2Le"> <a class="M3vVJe" href="https://www.google.com/url?q=https://support.google.com/websearch%3Fp%3Dfeatured_snippets%26hl%3Den-SG&opi=89978449&usg=AOvVaw0XmUePKqidLOPpq7KneD4H">About featured snippets</a> </span> </div></div></div> </div> </div><div> <div> <div class="ezO2md"><div><div><a class="fuLhoc ZWRArf" href="/url?q=https://en.wikipedia.org/wiki/Argument_of_latitude&sa=U&ved=2ahUKEwih4sDR_cuLAxW7SWwGHTUGAvcQFnoECAsQAg&usg=AOvVaw1diCy45ztwcND02caihQ0o"><span class="CVA68e qXLe6d fuLhoc ZWRArf">Argument of latitude - Wikipedia</span> <span class="qXLe6d dXDvrc"> <span class="fYyStc">en.wikipedia.org › wiki › Argument_of_latitude</span> </span> </a></div><div class="Dks9wf"><table class="KZhhub"><tr><td class="udTCfd"><div> <div> <span class="qXLe6d FrIlee"> <span class="fYyStc">It is the angle between the ascending node and the body. It is the sum of the more commonly used true anomaly and argument of periapsis.</span> </span> </div> </div></td></tr></table></div></div></div> </div> </div><div> <div> <div class="ezO2md"><div><div><table class="ZuwI5d"><tbody><tr><td> <span class="qXLe6d x3G5ab"> <span class="fYyStc">Argument of latitude</span> </span> </td><td><a href="/url?q=https://www.researchgate.net/figure/Relative-argument-of-latitude-The-orbit-radius-is-expressed-as_fig2_252454636&sa=U&ved=2ahUKEwih4sDR_cuLAxW7SWwGHTUGAvcQndQBegQICBAE&usg=AOvVaw19I8L_MqB-B0Lu4CKuqZ1h"><img class="qPa7sb" alt="Argument of latitude" src="https://encrypted-tbn0.gstatic.com/images?q=tbn:ANd9GcRX0HKpPmi86XboM_8pD5Vbfi6y-bDH_kiImuKa2O7FfffNz2P71JS1Z54&s=0" style="max-width:72px;max-height:72px"/></a></td></tr></tbody></table></div><div class="AS66f"> <div> <span class="qXLe6d FrIlee"> <span class="fYyStc">In celestial mechanics, the argument of latitude is an angular parameter that defines the position of a body moving along a Kepler orbit. It is the angle between the ascending node and the body. It is the sum of the more commonly used true anomaly...</span> <span class="fYyStc"> </span> <a class="M3vVJe" href="/url?q=https://en.wikipedia.org/wiki/Argument_of_latitude&sa=U&ved=2ahUKEwih4sDR_cuLAxW7SWwGHTUGAvcQmhN6BAgIEAY&usg=AOvVaw2E5cSVC9DwppVDxSlwuf52">Wikipedia</a> </span> </div> </div></div></div> </div> </div><div> <div> <div class="ezO2md"><div><div><a class="fuLhoc ZWRArf" href="/url?q=https://www.researchgate.net/figure/Relative-argument-of-latitude-The-orbit-radius-is-expressed-as_fig2_252454636&sa=U&ved=2ahUKEwih4sDR_cuLAxW7SWwGHTUGAvcQFnoECAkQAg&usg=AOvVaw2LcIeuQkUZl4J8_-4HTjY4"><span class="CVA68e qXLe6d fuLhoc ZWRArf">Relative argument of latitude The orbit radius is expressed as</span> <span class="qXLe6d dXDvrc"> <span class="fYyStc">www.researchgate.net › figure › Relative-argument-of-latitude-The-orbit-ra...</span> </span> </a></div><div class="Dks9wf"><table class="KZhhub"><tr><td class="udTCfd"><div> <div> <span class="qXLe6d FrIlee"> <span class="fYyStc">R is the argument of latitude relative to the intersection of the two orbit planes and r is the orbit radius.</span> </span> </div> </div></td></tr></table></div></div></div> </div> </div><div> <div> <div class="ezO2md"><div><div><a class="fuLhoc ZWRArf" href="/url?q=https://onelook.com/%3Floc%3Dolthes1%26w%3DArgument%2520of%2520latitude&sa=U&ved=2ahUKEwih4sDR_cuLAxW7SWwGHTUGAvcQFnoECAcQAg&usg=AOvVaw0Wmy4dOGtJSEHwutIh-XA9"><span class="CVA68e qXLe6d fuLhoc ZWRArf">ARGUMENT OF LATITUDE: Meaning and related words - OneLook</span> <span class="qXLe6d dXDvrc"> <span class="fYyStc">onelook.com › w=Argument of latitude</span> </span> </a></div><div class="Dks9wf"><table class="KZhhub"><tr><td class="udTCfd"><div> <div> <span class="qXLe6d FrIlee"> <span class="fYyStc">In celestial mechanics, the argument of latitude is an angular parameter that defines the position of a body moving along a Kepler orbit.</span> </span> </div> </div></td></tr></table></div></div></div> </div> </div><div> <div> <div class="ezO2md"><div><div><a class="fuLhoc ZWRArf" href="/url?q=https://colorado.pressbooks.pub/introorbitalmechanics/chapter/copy-of-chapter-3__editing/&sa=U&ved=2ahUKEwih4sDR_cuLAxW7SWwGHTUGAvcQFnoECAQQAg&usg=AOvVaw1Ib77ZWasMtCUFuUV1V_XI"><span class="CVA68e qXLe6d fuLhoc ZWRArf">Chapter 3 – The Classical Orbital Elements (COEs)</span> <span class="qXLe6d dXDvrc"> <span class="fYyStc">colorado.pressbooks.pub › chapter › copy-of-chapter-3__editing</span> </span> </a></div><div class="Dks9wf"><table class="KZhhub"><tr><td class="udTCfd"><div> <div> <span class="qXLe6d FrIlee"> <span class="fYyStc">Argument of latitude can take any value between 0° and 360° so a half plane check is needed. As can be seen in the figure above, if the kth component of the ...</span> </span> </div> </div></td></tr></table></div></div></div> </div> </div><div> <div> <div class="ezO2md"><div><div><a class="fuLhoc ZWRArf" href="/url?q=https://ocw.mit.edu/courses/16-346-astrodynamics-fall-2008/98996c87e2c8679bda5d37f7a3d7785c_lec_05.pdf&sa=U&ved=2ahUKEwih4sDR_cuLAxW7SWwGHTUGAvcQFnoECAMQAg&usg=AOvVaw0hBkWo5K1k-PxjMgplh2XS"><span class="CVA68e qXLe6d fuLhoc ZWRArf">[PDF] 16.346 Astrodynamics - MIT OpenCourseWare</span> <span class="qXLe6d dXDvrc"> <span class="fYyStc">ocw.mit.edu › courses › 16-346-astrodynamics-fall-2008</span> </span> </a></div><div class="Dks9wf"><table class="KZhhub"><tr><td class="udTCfd"><div> <div> <span class="qXLe6d FrIlee"> <span class="fYyStc">where θ = ω + f is called the argument of latitude. Terminology. #3.4, Page 160–161. Time of pericenter passage τ. Argument of latitude θ = ω + f. Angle of ...</span> </span> </div> </div></td></tr></table></div></div></div> </div> </div><div> <div> <div class="ezO2md"><div><div><a class="fuLhoc ZWRArf" href="/url?q=https://www.faa.gov/sites/faa.gov/files/about/office_org/headquarters_offices/avs/III.4.1.4_Describing_Orbits.pdf&sa=U&ved=2ahUKEwih4sDR_cuLAxW7SWwGHTUGAvcQFnoECAYQAg&usg=AOvVaw0mSdh2miNeLxdJcRYNzxtm"><span class="CVA68e qXLe6d fuLhoc ZWRArf">[PDF] Describing Orbits</span> <span class="qXLe6d dXDvrc"> <span class="fYyStc">www.faa.gov › office_org › avs › III.4.1.4_Describing_Orbits.pdf</span> </span> </a></div><div class="Dks9wf"><table class="KZhhub"><tr><td class="udTCfd"><div> <div> <span class="qXLe6d FrIlee"> <span class="fYyStc">We measure argument of latitude, u, along the orbital path from the ascending node to the spacecraft's position in the direction of the spacecraft's motion.</span> </span> </div> </div></td></tr></table></div></div></div> </div> </div><div> <div> <div class="ezO2md"><div><div><a class="fuLhoc ZWRArf" href="/url?q=https://www.researchgate.net/figure/Explanation-of-the-orbital-elements-inclination-i-argument-of-latitude-f-u_fig5_256115089&sa=U&ved=2ahUKEwih4sDR_cuLAxW7SWwGHTUGAvcQFnoECAEQAg&usg=AOvVaw1va9r5P1KaV6fDR2ZUj4E5"><span class="CVA68e qXLe6d fuLhoc ZWRArf">Explanation of the orbital elements: inclination i, argument of latitude fu</span> <span class="qXLe6d dXDvrc"> <span class="fYyStc">www.researchgate.net › figure › Explanation-of-the-orbital-elements-inclin...</span> </span> </a></div><div class="Dks9wf"><table class="KZhhub"><tr><td class="udTCfd"><div> <div> <span class="qXLe6d FrIlee"> <span class="fYyStc">The argument of latitude that defines the position of a body moving along a Kepler orbit, i its orbital inclination,  is the argument of the perigee of the ...</span> </span> </div> </div></td></tr></table></div></div></div> </div> </div><div> <div> <div class="ezO2md"><div><div><a class="fuLhoc ZWRArf" href="/url?q=https://gssc.esa.int/navipedia/index.php/Two-body_Problem&sa=U&ved=2ahUKEwih4sDR_cuLAxW7SWwGHTUGAvcQFnoECAUQAg&usg=AOvVaw0B8cmsDS0rMvUQ4lZOLUtA"><span class="CVA68e qXLe6d fuLhoc ZWRArf">Two-body Problem - Navipedia - GSSC</span> <span class="qXLe6d dXDvrc"> <span class="fYyStc">gssc.esa.int › navipedia › index.php › Two-body_Problem</span> </span> </a></div><div class="Dks9wf"><table class="KZhhub"><tr><td class="udTCfd"><div> <div> <span class="qXLe6d FrIlee"> <span class="fYyStc YVIcad">23 Feb 2012</span> <span class="fYyStc YVIcad"> · </span> <span class="fYyStc">The sum of the true anomaly and the argument of perigee defines the Argument of Latitude. Notice that for a circular orbit ( e = 0 ) the ...</span> </span> </div> </div></td></tr></table></div></div></div> </div> </div><div> <div> <div class="ezO2md"><div><div><a class="fuLhoc ZWRArf" href="/url?q=https://encyclopedia2.thefreedictionary.com/argument%2Bof%2Blatitude&sa=U&ved=2ahUKEwih4sDR_cuLAxW7SWwGHTUGAvcQFnoECAoQAg&usg=AOvVaw1n9xuwp5jALa_FIJ6BZ3HV"><span class="CVA68e qXLe6d fuLhoc ZWRArf">Argument of latitude - Encyclopedia - The Free Dictionary</span> <span class="qXLe6d dXDvrc"> <span class="fYyStc">encyclopedia2.thefreedictionary.com › argument+of+latitude</span> </span> </a></div><div class="Dks9wf"><table class="KZhhub"><tr><td class="udTCfd"><div> <div> <span class="qXLe6d FrIlee"> <span class="fYyStc">The angular distance measured in the orbit plane from the ascending node to the orbiting object; the sum of the argument of perigee and the true anomaly.</span> </span> </div> </div></td></tr></table></div></div></div> </div> </div><div> <div> <div class="ezO2md"><div><div> <span class="qXLe6d x3G5ab"> <span class="dloBPe fYyStc">Related searches</span> </span> </div><div><table class="VeHcBf"><tbody><tr><td><a class="ZWRArf" href="/search?sca_esv=bbb4249b07bbd0d1&q=argument+of+perigee&sa=X&ved=2ahUKEwih4sDR_cuLAxW7SWwGHTUGAvcQ1QJ6BAgAEAE"><span class="CVA68e qXLe6d"> <span class="qXLe6d FrIlee"> <span class="fYyStc">argument of perigee</span> </span> </span></a></td><td><div class="MGsU1d"><a href="/search?sca_esv=bbb4249b07bbd0d1&q=argument+of+perigee"><div class="FrIlee">></div></a></div></td></tr></tbody></table></div><div><table class="VeHcBf"><tbody><tr><td><a class="ZWRArf" href="/search?sca_esv=bbb4249b07bbd0d1&q=true+longitude&sa=X&ved=2ahUKEwih4sDR_cuLAxW7SWwGHTUGAvcQ1QJ6BAgAEAI"><span class="CVA68e qXLe6d"> <span class="qXLe6d FrIlee"> <span class="fYyStc">true longitude</span> </span> </span></a></td><td><div class="MGsU1d"><a href="/search?sca_esv=bbb4249b07bbd0d1&q=true+longitude"><div class="FrIlee">></div></a></div></td></tr></tbody></table></div><div><table class="VeHcBf"><tbody><tr><td><a class="ZWRArf" href="/search?sca_esv=bbb4249b07bbd0d1&q=argument+of+periapsis+ksp&sa=X&ved=2ahUKEwih4sDR_cuLAxW7SWwGHTUGAvcQ1QJ6BAgAEAM"><span class="CVA68e qXLe6d"> <span class="qXLe6d FrIlee"> <span class="fYyStc">argument of periapsis ksp</span> </span> </span></a></td><td><div class="MGsU1d"><a href="/search?sca_esv=bbb4249b07bbd0d1&q=argument+of+periapsis+ksp"><div class="FrIlee">></div></a></div></td></tr></tbody></table></div><div><table class="VeHcBf"><tbody><tr><td><a class="ZWRArf" href="/search?sca_esv=bbb4249b07bbd0d1&q=argument+of+perigee+calculation&sa=X&ved=2ahUKEwih4sDR_cuLAxW7SWwGHTUGAvcQ1QJ6BAgAEAQ"><span class="CVA68e qXLe6d"> <span class="qXLe6d FrIlee"> <span class="fYyStc">argument of perigee calculation</span> </span> </span></a></td><td><div class="MGsU1d"><a href="/search?sca_esv=bbb4249b07bbd0d1&q=argument+of+perigee+calculation"><div class="FrIlee">></div></a></div></td></tr></tbody></table></div><div><table class="VeHcBf"><tbody><tr><td><a class="ZWRArf" href="/search?sca_esv=bbb4249b07bbd0d1&q=orbital+argument&sa=X&ved=2ahUKEwih4sDR_cuLAxW7SWwGHTUGAvcQ1QJ6BAgAEAU"><span class="CVA68e qXLe6d"> <span class="qXLe6d FrIlee"> <span class="fYyStc">orbital argument</span> </span> </span></a></td><td><div class="MGsU1d"><a href="/search?sca_esv=bbb4249b07bbd0d1&q=orbital+argument"><div class="FrIlee">></div></a></div></td></tr></tbody></table></div><div><table class="VeHcBf"><tbody><tr><td><a class="ZWRArf" href="/search?sca_esv=bbb4249b07bbd0d1&q=longitude+of+ascending+node+calculator&sa=X&ved=2ahUKEwih4sDR_cuLAxW7SWwGHTUGAvcQ1QJ6BAgAEAY"><span class="CVA68e qXLe6d"> <span class="qXLe6d FrIlee"> <span class="fYyStc">longitude of ascending node calculator</span> </span> </span></a></td><td><div class="MGsU1d"><a href="/search?sca_esv=bbb4249b07bbd0d1&q=longitude+of+ascending+node+calculator"><div class="FrIlee">></div></a></div></td></tr></tbody></table></div><div><table class="VeHcBf"><tbody><tr><td><a class="ZWRArf" href="/search?sca_esv=bbb4249b07bbd0d1&q=longitude+of+periastron&sa=X&ved=2ahUKEwih4sDR_cuLAxW7SWwGHTUGAvcQ1QJ6BAgAEAc"><span class="CVA68e qXLe6d"> <span class="qXLe6d FrIlee"> <span class="fYyStc">longitude of periastron</span> </span> </span></a></td><td><div class="MGsU1d"><a href="/search?sca_esv=bbb4249b07bbd0d1&q=longitude+of+periastron"><div class="FrIlee">></div></a></div></td></tr></tbody></table></div><div><table class="VeHcBf"><tbody><tr><td><a class="ZWRArf" href="/search?sca_esv=bbb4249b07bbd0d1&q=moon+longitude+of+ascending+node&sa=X&ved=2ahUKEwih4sDR_cuLAxW7SWwGHTUGAvcQ1QJ6BAgAEAg"><span class="CVA68e qXLe6d"> <span class="qXLe6d FrIlee"> <span class="fYyStc">moon longitude of ascending node</span> </span> </span></a></td><td><div class="MGsU1d"><a href="/search?sca_esv=bbb4249b07bbd0d1&q=moon+longitude+of+ascending+node"><div class="FrIlee">></div></a></div></td></tr></tbody></table></div></div></div> </div> </div></div><table class="uZgmoc"><tbody><td><a class="frGj1b" href="/search?q=argument+of+latitude&sca_esv=bbb4249b07bbd0d1&ei=ZdazZ-GbJruTseMPtYyIuA8&start=10&sa=N">Next ></a></td></tbody></table><br/><div class="TuS8Ad" data-ved="0ahUKEwih4sDR_cuLAxW7SWwGHTUGAvcQpyoIQg"><style>.VYM29{font-weight:bold}</style><div class="HddGcc" align="center"><span class="VYM29">Singapore</span><span> - </span><span>From your IP address</span><span> - </span><a href="/url?q=https://support.google.com/websearch%3Fp%3Dws_settings_location%26hl%3Den-SG&opi=89978449&sa=U&ved=0ahUKEwih4sDR_cuLAxW7SWwGHTUGAvcQty4IQw&usg=AOvVaw3XSml2VM7Q4b5inOhSyKcX">Learn more</a></div><div align="center"><a class="rEM8G" href="/url?q=https://accounts.google.com/ServiceLogin%3Fcontinue%3Dhttps://www.google.com/search%253Fsca_esv%253Dbbb4249b07bbd0d1%2526q%253Dargument%252Bof%252Blatitude%26hl%3Den&opi=89978449&sa=U&ved=0ahUKEwih4sDR_cuLAxW7SWwGHTUGAvcQxs8CCEQ&usg=AOvVaw0VxvJ79MlcrqrOSZhEfOpr">Sign in</a></div><div><table class="bookcf"><tbody class="InWNIe"><tr><td><a class="rEM8G" href="https://www.google.com/preferences?hl=en&sa=X&ved=0ahUKEwih4sDR_cuLAxW7SWwGHTUGAvcQv5YECEU">Settings</a></td><td><a class="rEM8G" href="https://www.google.com/intl/en_sg/policies/privacy/">Privacy</a></td><td><a class="rEM8G" href="https://www.google.com/intl/en_sg/policies/terms/">Terms</a></td></tr></tbody></table></div></div><div> </div></body></html>