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
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
| 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 |
-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 !!!
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