ephemerisCompute
is a command-line tool for producing tables of the positions
of solar system objects over time.
For the Sun, Moon and planets, it extracts positions from the publicly available NASA DE430 ephemeris (published 2013), which covers the time period 1550 to 2650 AD, typically with an accuracy of a few km. Outside of this time range, it solves Kepler's equation for the position of an object in an elliptical orbit, yielding results of much lower accuracy.
For asteroids, it solves Kepler's equation using orbital elements downloaded
from Ted Bowell's astorb.dat
catalogue.
For comets, it obtains orbital elements from the Minor Planet Center's website.
ephemerisCompute
was written to produce all the ephemerides on the website
https://in-the-sky.org, which is maintained by the author.
An older version of this tool is also available, which uses the NASA DE405 ephemeris (published 1997).
ephemerisCompute
is written in C and runs in Linux, MacOS, and other
Unix-like operating systems.
This code is distributed under the Gnu General Public License. It is (C) Dominic Ford 2010 - 2024.
Before you start, ephemerisCompute
needs to download various data from the
internet, including the DE430 ephemeris files, the asteroid catalogue, and the
list of comets.
This can be done with the shell script setup.sh
. The total download size will
be around 500 MB.
Note that once you have built ephemerisCompute
, you must not change its location
within your file system. During the build process, the absolute path to the
downloaded data files is stored, and the code will be unable to find these data
files if their path changes. If you move the code, you must fully rebuild the
code:
make clean
./setup.sh
A Dockerfile
is provided to build ephemerisCompute
. A docker compose
script is
provided to build a selection of example starcharts:
docker compose build
docker compose run ephemeris-compute-de430
This produces a single demo ephemeris. To make other ephemerides, open a shell within the Docker container as follows:
docker run -it ephemeris-compute-de430:v4 /bin/bash
Running the command-line tool bin/ephem.bin
will produce a default ephemeris
for Jupiter between 2000 Jan 1 and 2000 Feb 1, at midnight each day:
dominic@ganymede:~/ephemerisCompute$ ./bin/ephem.bin
2451544.500000000000 3.996320681 2.730993728 1.073274469
2451545.500000000000 3.991757746 2.736868431 1.075903739
2451546.500000000000 3.987185148 2.742736516 1.078530407
...
The first time you run the tool, it needs to convert the ASCII data files you downloaded into a binary format, which will typically take a few seconds before any output is produced. The binary data is cached, leading to near instantaneous performance subsequently.
In this output, the columns are Julian day number, and the XYZ position of Jupiter, measured in AU, relative to the centre of mass of the solar system.
The following command-line arguments can be used to customise the ephemeris:
--jd_min
[float] - Specify the Julian day number at which the ephemeris should begin.
--jd_max
[float] - Specify the Julian day number at which the ephemeris should end.
--jd_step
[float] - Specify the interval between the lines in the ephemeris, in days.
--latitude
[float] - The latitude of the observation site (deg); only used if topocentric correction enabled.
--longitude
[float] - The longitude of the observation site (deg); only used if topocentric correction enabled.
--enable_topocentric_correction
[int] - Set to either 0 (return geocentric coordinates) or 1 (return topocentric coordinates).
--epoch
[float] - Specify the epoch of the RA/Dec coordinate system, e.g. 2451545.0 for J2000 (default).
--objects
[string] - Specify the list of objects to produce ephemerides for. Objects should be separated by commas, e.g. "jupiter, mars" or "P301, A4, 1P/Halley". See below for an explanation of what names are accepted for objects. If multiiple objects are listed, their positions are listed in sets of columns from left to right.
--output_binary
[int] - If zero, a text-based ephemeris is produced. If non-zero, then the data is output as a stream of binary data, with type double
. The first column, the Julian day number, is omitted from binary ephemerides.
--output_constellations
[int] - If non-zero, then the final column states the name of the constellation the object is in. Note the fetching this information is one of the slowest routines within ephemerisCompute, so this may have significant performance impact when computing large ephemerides.
--use_orbital_elements
[int] - If zero, then the NASA JPL DE430 ephemeris is used to produce the ephemeris. This will give best accuracy (by far). If set to 1, then orbital elements for all objects are used to compute their approximate positions. If set to 2, then algorithms from Jean Meeus's book "Astronomical Algorithms" are used [not currently supported; do not use!]. The positions of comets and asteroids are always computed using orbital elements, since they are not included in DE430.
--output_format
[int] - Selects what data should be returned. The following formats are currently supported:
This section lists the names which are recognised by the --objects
command-line argument:
p1
, pmercury
, mercury
: Mercuryp2
, pvenus
, venus
: Venusp3
, pearth
, earth
: Earthp301
, pmoon
, moon
: The Moonp4
, pmars
, mars
: Marsp5
, pjupiter
, jupiter
: Jupiterp6
, psaturn
, saturn
: Saturnp7
, puranus
, uranus
: Uranusp8
, pneptune
, neptune
: Neptunep9
, ppluto
, pluto
: PlutoA<n>
: Asteroid number n
, e.g. A1
for Ceres, or A4
for VestaC/1995 O1
. Comets may be referred to by their names in this format1P/Halley
. Comets may be referred to by their names in this format0001P
. Periodic comets may be referred to by their names in the format %4dPCJ95O010
. Comets may be referred to by their Minor Planet Center designationsC<n>
: Comer number n
. n
is the line number within the file Soft00Cmt.txt, downloaded from the Minor Planet Center.Version 4.0 (23 Sept 2024) - Added optional topocentric correction.
Version 3.0 (23 Aug 2024) - Added corrections for light travel time and annual aberration. Improvements to numerical stability when calculating hyperbolic orbits.
Version 2.0 (16 Oct 2022) - Initial public release.
This code was developed by Dominic Ford https://dcford.org.uk. It is distributed under the Gnu General Public License V3.