Computer Ephemeris . ... Content of the Computer Ephemeris is the same as content of Soviet Astronomical Almanac (Ezhegodnik), but fully original algorithms and computer methods of calculations were used. Your requests for Computer Ephemeris for years before 2014 and your comments on its contents please direct to the author charlie@mail.univ.kiev.ua . ... Keywords: Computer Ephemerides, Computer Ephemeris, Computer Almanac, Computer Calendar. ...
. Computer Ephemeris for 2016 from DE200/LE200. Map of the Lunar eclipse - 18 Aug 2016. There is mercator global map of the world with eclipse lines on it. Legend: Curved lines are for eclipse limits in the horizon red line is for semishadow eclipse, blue line is for shadow eclipse, yellow line is for total eclipse. Straight line connects the sub-Lunar points during the eclipse (sorry, but it's yellow too).
. Computer Ephemeris for 2016 from DE200/LE200. Map of the Solar eclipse - 09 Mar 2016. =1.0 violet lines are for isohrones (every exact half of hour). Please use ordinal common sence to orient yourself in the map. Mercator global view. Stereographic global map.
Computer Ephemeris for 2016 from DE200/LE200. First page. Epoch T = J2016.5 = date 2016 Jul 2.125 (JD2457571.625) = besselian epoch B2016.50163 Beginning of spring: Mar 20 4 h 31.22 m summer: Jun 20 22 h 35.23 m autumn ... Sep 22 14 h 22.28 m winter: Dec 21 10 h 45.28 m Earth in perihelion: Jan 02 22.83 h aphelion : Jul 04 16.42 h Mean obliquity of ecliptic ( eps ) at J2016.5 : 23.437145 o = 23 o 26 ' 13.72 Sin( eps ) = 0.39774280 Cosec( eps ) = 2.51418758 Cos( eps ) = 0.91749696 Sec( ...
Computer Ephemeris for 2016 from DE200/LE200. Elements of the Partial Lunar eclipse - 23 Mar 2016. 2016 Mar 23 11 h 4 m 35.50 s Min(gamma) = 1.15604 t = time - 11 h 0 m Geocentric coordinates of the Sun: Right ascension = 1154.626 + t * 9.101 Declination = 11723.384 + t * 59.065 + t * t * -0.002 Parallax = 8.822 Radius = 1602.693 + t * -0.012 Geocentric coordinates of the Moon: Right ascension = 121147.116 + t * 153.476 + t * t * - ...
Computer Ephemeris for 2016 from DE200/LE200. Reduction quantities ( dynamical time scale). tau A+A' B+B' C D E A' B' a 0s0001 0 001 0 001 Jan 1 -0.5014 -10.385 9.742 -3.321 20.516 -1 18 -74 2 -0.4986 -10.351 9.736 -3.650 20.451 -1 -16 -72 3 -0.4959 -10.315 9.742 -3 tau A+A' B+B' C D E A' B' a 0s0001 0 001 0 001 Feb 1 -0.4165 -8.602 9.293 -12.532 15.675 -1 -80 -15 2 -0.4138 -8.554 9.303 -12.781 15.433 -1 -84 17 3 -0.4110 -8.495 9.311 -13 ...
Computer Ephemeris for 2016 from DE200/LE200. Lunar orbital data. Date M e a n e q u a t o r O r b i t i delta OMEGA' ѓ' OMEGA longitude Dec 24 24.9735 356.2631 359.7472 13.4485 176.0329 69.1780 Jan 3 24.9725 355.7644 359.7136 14.5625 175.5033 200.9420 13 24.9714 355 ... .2775 358.5645 53.5537 156.9695 132.6808 28 24.8556 337.7768 358.5331 54.6677 156.4400 264.4447 Daily movements (degrees) of Mean longitude of perigee = 0.111403 Mean ...
Computer Ephemeris for 2016 from DE200/LE200. Equatorial positions of the Moon . date alpha delta distance h m s o ' Jan 1.0 114806.624 12745.72 63.1545985 1.5 121041.241 -2443.16 63.2820830 2.0 123311.704 -21633.38 63.3592196 2.5 125543.308 -40653.03 63.3847579 3.0 131821.254 -55450.50 ...
Computer Ephemeris for 2016 from DE200/LE200. ... 2016 Sep 16 18 h 18 m 28.12 s Min(gamma) = 1.05314 t = time - 18 h 10 m Geocentric coordinates of the Sun: Right ascension = 113902.919 ... t * t * 0.868 Parallax = 10005.808 + t * 1.243 + t * t * -0.012 Radius = 1622.511 + t * 0.339 + t * t * -0.004 Contacts of the eclipse : Begin Semishadow eclipse : 16 53.93 Phase Maximum of eclipse : 18 55.54 End Semishadow eclipse : 20 57.06 Elements of the lunar ...