Ephemerides 2026 May Module


 Overview
 

1°)  Ecliptic Geocentric Coordinates
2°)  Equatorial Geocentric Coordinates
3°)  Azimuthal Topocentric Coordinates
4°)  Numerical Results


-These programs compute accurate positions of the Sun, the Moon and the major planets ( this month, not enough room for Pluto )
    for a short time-span of 32 days, i-e  2026/04/30 0h TT to 2026/06/01  0h TT

-The longitudes & latitudes and the right-ascensions & declinations are geocentric apparent
  referred to the true equator & equinox of the date, corrected for aberration and light-time.

-The precision is about 0"01 for the longitudes & latitudes and of the order of 3 E-8 AU for the distances ( 5 E-11 AU for the Moon ).
-The distances are true distances.

-The azimuthal ( topocentric ) coordinates are also given, corrected for parallax & diurnal aberration.

-These coordinates are calculated by polynomials fitted to the JPL Ephemerides DE441
 

Notes:

-Always execute "ECL" first for the ecliptic coordinates, with at least SIZE 031
-Then "EQ" for the equatorial coordinates ( SIZE 039 )
-And then "AZ" for the azimuthal coordinates with at least SIZE 041.

-The azimuths are reckoned clockwise from North.
-Longitudes are positive East.
 

Data Registers

  R00 = ( DOM - 16 ) / 16 ( from -1  to +1 )  Terrestrial Time ( TT )

  R01 thru R30 = coordinates of the Sun, the Moon, Mercury, Venus, Mars, Jupiter, Saturn, Uranus, Neptune & Pluto.

  R31 = True obliquity of the ecliptic  ( deg )
  R32 = Local Sidereal Time  ( hh.mnss )

 • R33 = Longitude of the observer ( ° ' " )   positive East
 • R34 = Latitude of the observer ( ° ' " )                                                         Registers R33-R34-R35 are to be initialized before executing "AZ"
 • R35 = Observer altitude in meters

 ( R36 to R40:  temporary data storage )
 
 

XROM  Function  Desciption
 24,00
 24,01
 24,02
 24,03
 24,04
 24,05
 S
-EPH2026MAY
 V
 ECL
 EQ
 AZ
 Subroutine that is called by "V"
 Section Header
 Ecliptic Coordinates of the Sun, the Moon & the Planets

 Takes day of month & time and calls "V"
 Ecliptic -> Equatorial Coordinates
 Equatorial -> Azimuthal Coordinates
  


-"ECL"  "EQ"  &  "AZ"  calculate & store the coordinates in registers R01 thru R27 as follows:

>>>   h0 is the height, corrected for refraction
 
 

      Celestial Body    Registers                  "ECL"                  "EQ"            "AZ"
            SUN       R01
      R02
      R03
    Eclipt Longitude ( deg )
    Eclipt  Latitude ( deg )
    Dist from Earth ( AU )
    Right-Ascens(hh;mnss)
      Declination ( ° ' " )
    Dist from Earth ( AU )
   Azimuth ( ° ' " )
     height  ( ° ' " )
        h0  ( ° ' " )
          MOON       R04
      R05
      R06
    Eclipt Longitude ( deg )
    Eclipt  Latitude ( deg )
    Dist from Earth ( AU )
    Right-Ascens(hh;mnss)
      Declination ( ° ' " )
    Dist from Earth ( AU )
    Azimuth ( ° ' " )
     height  ( ° ' " )
        h0  ( ° ' " )
       MERCURY       R07
      R08
      R09
    Eclipt Longitude ( deg )
    Eclipt  Latitude ( deg )
    Dist from Earth ( AU )
    Right-Ascens(hh;mnss)
      Declination ( ° ' " )
    Dist from Earth ( AU )
    Azimuth ( ° ' " )
     height  ( ° ' " )
        h0  ( ° ' " )
         VENUS       R10
      R11
      R12
    Eclipt Longitude ( deg )
    Eclipt  Latitude ( deg )
    Dist from Earth ( AU )
   Right-Ascens(hh;mnss)
     Declination ( ° ' " )
   Dist from Earth ( AU )
    Azimuth ( ° ' " )
     height  ( ° ' " )
        h0  ( ° ' " )
          MARS       R13
      R14
      R15
    Eclipt Longitude ( deg )
    Eclipt  Latitude ( deg )
    Dist from Earth ( AU )
    Right-Ascens(hh;mnss)
      Declination ( ° ' " )
   Dist from Earth ( AU )
    Azimuth ( ° ' " )
     height  ( ° ' " )
        h0  ( ° ' " )
        JUPITER       R16
      R17
      R18
    Eclipt Longitude ( deg )
    Eclipt  Latitude ( deg )
    Dist from Earth ( AU )
    Right-Ascens(hh;mnss)
      Declination ( ° ' " )
    Dist from Earth ( AU )
    Azimuth ( ° ' " )
     height  ( ° ' " )
        h0  ( ° ' " )
        SATURN       R19
      R20
      R21
    Eclipt Longitude ( deg )
    Eclipt  Latitude ( deg )
    Dist from Earth ( AU )
    Right-Ascens(hh;mnss)
      Declination ( ° ' " )
    Dist from Earth ( AU )
    Azimuth ( ° ' " )
     height  ( ° ' " )
        h0  ( ° ' " )
        URANUS       R22
      R23
      R24
    Eclipt Longitude ( deg )
    Eclipt  Latitude ( deg )
    Dist from Earth ( AU )
    Right-Ascens(hh;mnss)
      Declination ( ° ' " )
    Dist from Earth ( AU )
    Azimuth ( ° ' " )
     height  ( ° ' " )
        h0  ( ° ' " )
       NEPTUNE       R25
      R26
      R27
    Eclipt Longitude ( deg )
    Eclipt  Latitude ( deg )
    Dist from Earth ( AU )
    Right-Ascens(hh;mnss)
      Declination ( ° ' " )
    Dist from Earth ( AU )
    Azimuth ( ° ' " )
     height  ( ° ' " )
        h0  ( ° ' " )

 

1°) Ecliptic Geocentric Coordinates of the Sun, the Moon & the major Planets


            STACK            INPUTS      OUTPUTS
                 Z                 /       R0  ( AU )
                 Y       Day of the Month       B0  ( deg )
                 X        HH.MNSS(TT)       L0  ( deg )

    Where  L = Longitude   B = Latitude   R = radius vector

Example:    Calculate the apparent geocentric ecliptic coordinates of the Sun, the Moon and the planets on 2026/05/24 at 16h41m  TT


-Enter the day of the month and the time expressed in  Terrestrial Time ( TT )

       24       ENTER^
    16.41     XEQ "ECL"            >>>>     L0 =   63°528385           = R01                   
                                                RDN      B0 =   -0°000039            = R02
                                                RDN      R0 =  1.01266976  AU   = R03

Notes:

-All the angles are expressed in decimal degrees.
-Cf  paragraph 4°) for the other results.

-If you key in a date outside the interval [ 2026/04/30 0h TT , 2026/06/01   0h TT ]  you'll get a DATA ERROR message.
-However, this program may probably be used a few hours outside the prescribed interval: set F25 and R/S
-But the precision is less guaranteed and the results may even become completely meaningless several days before 00 or after 32, especially for the Moon.
 

2°) Equatorial Geocentric Coordinates
 

-AFTER executing "ECL", use "EQ" to get the equatorial coordinates
-The right-ascensions are expressed in hh.mnss and the declinations in ° ' "
-They replace the ecliptic longitudes & latitudes ( cf the tableau in the paragraph above )

-"EQUA" also calculates the true obliquity of the ecliptic which is returned in Z-register
-A polynomial is also used for that.
 
 

           STACK          INPUTS        OUTPUTS
               Z               /        eps   ( deg )
               Y               /       Decl0 ( ° ' " )
               X               /     RA0  ( hh.mnss )

  Where  RA = Right-Ascension   Decl = declination  eps = true obliquity of the ecliptic

Example:    Calculate the apparent geocentric equatorial coordinates of the Sun, the Moon and the planets on 2026/05/24 at 16h41m  TT

After executing "ECLI"


       XEQ "EQ"  or simply R/S if you've just executed "ECL"

                           >>>>     RA0 =       4h06m02s24     = R01              
                            RDN    Decl 0 =    20°51'29"06      = R02
                            RDN      eps  =     23°438075        = R31
 

-The distances in R03-R06-.....-R27  are unchanged.  
-Cf paragraph 4°) for the other results 


3°) Azimuthal Topocentric Coordinates
 

-AFTER executing "ECL" & "EQ" use "AZ" to get the horizontal coordinates
-The azimuths & heights are expressed in ° ' "

-The heights corrected for refraction are also computed and replace the distances in R03  R06 ..... R27
 
 

      STACK        INPUTS      OUTPUTS
           Z             /       h0  ( ° ' " )
           Y             /       h  ( ° ' " )
           X             /      Az  ( ° ' " )

                  Long = longitude ( positive East )       Az = Azimuth ( clockwise from North )    |
  Where       Lat  =  latitude                                   h  =  height                                             >       of the Sun
                   Alt  =  altitude in meters                   h0 =  height ( corrected for refraction )    |

Example:    Calculate the apparent topocentric azimuthal coordinates of the Sun, the Moon and the planets on 2026/05/24  at 16h41m  TT
                    at the Palomar Observatory,   Longitude = 116°51'50"4 W   Latitude = 33°21'22"4 N   Altitude = 1706 m
 

>>>  After executing "ECLI" & "EQUA"


    -116.51504   STO 33
       33.21224   STO 34
          1706       STO 35    R/S         >>>>      Az   =  94°59'11"14   = R01          
                                                        RDN         h   =  47°27'36"46    = R02
                                                       

         which are the topocentric coordinates of the Sun.
 

>>>  We also have the local sidereal time in R32 = LST = 23h03m17s48
 

Notes:

-Cf paragraph 4°) for the other results.
-The difference TT - UTC = 69.184 seconds. 

->  h0   is often meaningless when  h <   0
 

4°) Numerical Results

-Longitudes & latitudes are expressed in decimal degrees   and the distances in Astronomical Units ( "ECL" )
-Right-ascensions in hh.mnss & declinations in ° ' "  ( "EQ"   )
-Azimuths & heights in ° ' "  too   ( "AZ" )
  
-Obliquity of the ecliptic  in decimal degrees ( R31 )
-Local sidereal time in hh.mnss  ( R32 )



           Celestial Body    Registers          "ECL"          "EQ"          "AZ"
                 SUN       R01
      R02
      R03
     63.528385
     -0.000039
    1.01266976
     4.060224
    20.512906
    unchanged
    94.591114
    47.273646
    unchanged
               MOON       R04
      R05
      R06
    168.389201
     -1.194868
  0.0025900728
    11.152552
     3.293013
    unchanged
    39.265867
   -46.045772
    unchanged
            MERCURY       R07
      R08
      R09
     75.417276
      1.682383
    1.23063529
     4.555251
    24.184531
    unchanged
    83.560007
    38.330352
    unchanged
              VENUS       R10
      R11
      R12
     96.736260
      1.763786
    1.30297733
     6.294430
    25.014148
     unchanged
    72.245557
    19.425970
    unchanged
              MARS       R13
      R14
      R15
     34.321526
     -0.695175
    2.19994525
      2.091244
     12.181935
     unchanged
   139.462563
    63.533534
    unchanged
             JUPITER       R16
      R17
      R18
    112.721990
      0.406482
    5.86891087
      7.382525
     21.552886
     unchanged
    66.443647
     4.393531
    unchanged
             SATURN       R19
      R20
      R21
     11.597824
     -2.236086
   10.06455419
      0.460924
      2.314062
     unchanged
  -172.310349
    58.574068
    unchanged
            URANUS       R22
      R23
      R24
     61.638715
     -0.160258
    20.47665593
      3.581515
     20.195250
     unchanged 
    96.564562
    48.500813
    unchanged
            NEPTUNE       R25
      R26
      R27
      3.907951
     -1.334941
    30.38038475
     0.162791
     0.194119
    unchanged
  -159.541539
    55.184918
    unchanged
  True obliquity of the ecliptic       R31
           /
    23.438075
    unchanged
      Local Sidereal Time
      R32
           /
             /
   23.031748

 
    
5°) V

 

-This subroutine may be used for itself to calculate the geocentric ecliptic coordinates
-First initialize R00 before executing "V".
 
 -With the example above,  R00 = 0.5434461806


WARNING !!!


-Unlike "ECL" , this routine does not check if R00 is between -1 and +1

 6°)  Refraction


-This month, not enough room to compute the refraction. 


References:

[1]  Aldo Vitagliano SOLEX  http://www.solexorb.it/
[2]  ftp://ssd.jpl.nasa.gov/pub/eph/planets/ascii/
[3]  Jean Meeus - "Astronomical Algorithms" - Willmann-Bell  -  ISBN 0-943396-61-1