{"version":"1.0","provider_name":"SparkOne() Labs Official Site","provider_url":"https:\/\/sparkonelabs.com\/home","author_name":"admin","author_url":"https:\/\/sparkonelabs.com\/home\/author\/admin\/","title":"Planetary Orbital Mechanics (Demo.html) - SparkOne() Labs Official Site","type":"rich","width":600,"height":338,"html":"<blockquote class=\"wp-embedded-content\" data-secret=\"N39Nw9m36m\"><a href=\"https:\/\/sparkonelabs.com\/home\/2023\/11\/14\/planetary-orbital-mechanics-demo-html\/\">Planetary Orbital Mechanics (Demo.html)<\/a><\/blockquote><iframe sandbox=\"allow-scripts\" security=\"restricted\" src=\"https:\/\/sparkonelabs.com\/home\/2023\/11\/14\/planetary-orbital-mechanics-demo-html\/embed\/#?secret=N39Nw9m36m\" width=\"600\" height=\"338\" title=\"&#8220;Planetary Orbital Mechanics (Demo.html)&#8221; &#8212; SparkOne() Labs Official Site\" data-secret=\"N39Nw9m36m\" frameborder=\"0\" marginwidth=\"0\" marginheight=\"0\" scrolling=\"no\" class=\"wp-embedded-content\"><\/iframe><script>\n\/*! This file is auto-generated *\/\n!function(d,l){\"use strict\";l.querySelector&&d.addEventListener&&\"undefined\"!=typeof URL&&(d.wp=d.wp||{},d.wp.receiveEmbedMessage||(d.wp.receiveEmbedMessage=function(e){var t=e.data;if((t||t.secret||t.message||t.value)&&!\/[^a-zA-Z0-9]\/.test(t.secret)){for(var s,r,n,a=l.querySelectorAll('iframe[data-secret=\"'+t.secret+'\"]'),o=l.querySelectorAll('blockquote[data-secret=\"'+t.secret+'\"]'),c=new RegExp(\"^https?:$\",\"i\"),i=0;i<o.length;i++)o[i].style.display=\"none\";for(i=0;i<a.length;i++)s=a[i],e.source===s.contentWindow&&(s.removeAttribute(\"style\"),\"height\"===t.message?(1e3<(r=parseInt(t.value,10))?r=1e3:~~r<200&&(r=200),s.height=r):\"link\"===t.message&&(r=new URL(s.getAttribute(\"src\")),n=new URL(t.value),c.test(n.protocol))&&n.host===r.host&&l.activeElement===s&&(d.top.location.href=t.value))}},d.addEventListener(\"message\",d.wp.receiveEmbedMessage,!1),l.addEventListener(\"DOMContentLoaded\",function(){for(var e,t,s=l.querySelectorAll(\"iframe.wp-embedded-content\"),r=0;r<s.length;r++)(t=(e=s[r]).getAttribute(\"data-secret\"))||(t=Math.random().toString(36).substring(2,12),e.src+=\"#?secret=\"+t,e.setAttribute(\"data-secret\",t)),e.contentWindow.postMessage({message:\"ready\",secret:t},\"*\")},!1)))}(window,document);\n\/\/# sourceURL=https:\/\/sparkonelabs.com\/home\/wp-includes\/js\/wp-embed.min.js\n<\/script>\n","description":"Well these tabs are still open in the browser, so I might as well organize and prepare this information for implementation as part of demo.html. The basic idea here is that celestial bodies, whether large or small, have kinetic trajectories determined by the Kepler equation and another mode is used for when a significant perturbation","thumbnail_url":"https:\/\/i.stack.imgur.com\/nd58V.jpg?s=64&amp;g=1"}