B/astorb Orbits of Minor Planets (Bowell+, 2014-)
The Asteroid Orbital Elements Database, version 2022-Dec-12
Bowell E., Wasserman L., Moskovitz N., Burt B., Schottland R.
<Lowell Observatory (1999-2014)>
ADC_Keywords: Minor planets
Abstract:
astorb is a database of osculating orbital elements and ephemeris
uncertainties near the current epoch for all known asteroids in the Solar
System. It has been hosted at Lowell Observatory since the 1990's and is
actively curated to be automatically updated as new objects are discovered.
Access to the database, additional documentation, additional data, and
associated tools are available at asteroid.lowell.edu.
Introduction:
The file provided here is an ASCII summary of the database, with each object
occupying a 266 column record. Orbits are computed based on fits to
astrometric data downloaded from the Minor Planet Center.
There are several key features of the astorb database. (1) The database is
updated daily. Observations in each new batch of Minor Planet Circulars are
used to compute new orbits on a monthly basis, and those in the Minor Planet
Electronic Circulars shortly after they are published. Other updates, such
as the computation of current ephemeris uncertainties, are being made on a
quasi-daily basis. (2) All of the orbits in a given version of the file
have an epoch of osculation within 50 days of the present. Consequently, the
ephemerides of most non-planet-approaching asteroids can be computed to
arcsec accuracy or better within ± 50 days of the epoch using a 2-body
ephemeris program. (3) Current and future ephemeris uncertainties are given.
Observers will readily be able to estimate whether asteroids are likely to
be within their telescope's fields of view, and they will better be able to
prioritize astrometric targets.
To produce the database, our variable-timestep differential orbit correction
program was run in an automatic mode. Perturbation due to all major planets
(Mercury through Pluto, Earth and Moon separately), 1 Ceres, 2 Pallas,
3 Juno, 4 Vesta, 10 Hygiea, 15 Eunomia, 31 Euphrosyne, 52 Europa,
511 Davida, and 704 Interamnia were included. Planetary positions were
derived from JPL's DE430 planetary ephemeris. Positions of the perturbing
asteroids were derived, by iteration, from our own orbits. Relativistic
effects have been included. For Near Earth Objects, perturbations due to the
Earth's J2 have been included.
For the vast majority of asteroids the threshold for inclusion or exclusion
of observations in orbit determination is where the great-circle sky-plane
residuals exceed 2.3 arc seconds. In rare cases observations with higher
residuals are manually accepted. In no cases are residuals greater than
10 arc seconds accepted. Generally higher residuals are accepted from older,
pre-CCD data that offer significant arc extension.
Acknowledgment and Attribution:
The resources to support astorb.dat were originally provided by NASA grant
NAG5-4741 (PI E. Bowell) and the Lowell Observatory endowment, and more
recently by NASA PDART grant NNX16AG52G (PI N. Moskovitz). astorb.dat may
be freely used, copied, and transmitted provided attribution is made to the
aforementioned funding sources.
See also:
http://asteroid.lowell.edu/ : The Astorb database at Lowell Obs.
B/comets : Database of orbital elements of comets (Rocher, 2007)
II/190 : IRAS Minor Planet Survey (Tedesco 1992)
File Summary:
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FileName Lrecl Records Explanations
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ReadMe 80 . This file
astorb.dat 276 1078400 The catalog of Orbits
astorb.html 80 821 Introductory text to "astorb.dat" (HTML version)
astorb.txt 78 445 Introductory text to "astorb.dat" (plain ascii)
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Byte-by-byte Description of file: astorb.dat
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Bytes Format Units Label Explanations
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1- 6 I6 --- Planet [1,]?+ Asteroid number (blank if unnumbered)
8- 25 A18 --- Name Name or preliminary designation.
27- 41 A15 --- CompName Orbit Computer.
43- 47 F5.2 mag H Absolute magnitude H parameter (1)
49- 53 F5.2 --- G Slope magnitude parameter (1)
55- 58 F4.2 mag B-V ? Color index (see E.F.Tedesco, pp.1090-1138)
60- 64 F5.1 km Diam ? IRAS diameter (see E.F.Tedesco,
pp.1151-1161; catalog II/190)
66- 69 A4 --- IRAScl IRAS Taxonomic classification
72- 74 I3 --- Xflg [0/31] Planet-crossing code (4)
76- 78 I3 --- Oflg [0/255] Orbit computation code (5)
80- 82 I3 --- Sflg [0/31] Survey observation code (6)
84- 86 I3 --- MPCC [0/7] MPC critical-list code (7)
88- 90 I3 --- LowC [0/5] Lowell Observatory discovery code (8)
92- 94 I3 --- FlaC [0/10] Flagstaff Station Code (9)
96-100 I5 --- Narc ? Orbital arc, days, spanned by observations
used in orbit computation.
102-105 I4 --- Nobs Number of observations used in orbit
computation.
107-114 A8 "YYYYMMDD" Epoch Epoch of osculation, yyyymmdd (TDT) (2)
116-125 F10.6 deg M Mean anomaly (3)
127-136 F10.6 deg omega Argument of perihelion (3)
138-147 F10.6 deg Omega Longitude of ascending node (3)
148-157 F10.6 deg i Inclination (3)
159-168 F10.8 --- e Eccentricity (3)
169-181 F13.8 AU a ? Semimajor axis (3)
183-190 I8 "YYYYMMDD" DateOrb Date of orbit computation
192-198 E7.1 arcsec CEU ?=0 Current Ephemeris Uncertainty (10)
200-207 E8.1 arcsec/d dCEU ?=0 Rate of change of CEU (10)
209-216 I8 "YYYYMMDD" DateCEU ?=0 Date of CEU
218-224 E7.1 arcsec PEU0 ?=0 Next Peak Ephemeris Uncertainty (PEU) (11)
226-233 I8 "YYYYMMDD" DatePEU0 ?=0 Date of PEU0
235-241 E7.1 arcsec PEU1 ?=0 Largest PEU in 10 years from DatePEU0 (11)
243-250 I8 "YYYYMMDD" DatePEU1 ?=0 Date of PEU1
252-258 E7.1 arcsec PEU2 ?=0 As PEU1, assuming that two observations
were made at DatePEU0 (11)
260-267 I8 "YYYYMMDD" DatePEU2 ?=0 Date of PEU2
268 A1 --- mod [a*] added or updated (12)
269-276 I8 "YYYYMMDD" modDate ? Date of last modification (12)
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Note (1):
Absolute magnitude H, mag [see E. Bowell et al., pp. 549-554, in
"Asteroids II", R. P. Binzel et al. (eds.), The University of Arizona
Press, Tucson, 1989 and more recent Minor Planet Circulars].
Note that H may be given to 2 decimal places (e.g., 13.41), 1 decimal
place (13.4) or zero decimal (13.), depending on its estimated
accuracy. H is given to two decimal places for all unnumbered
asteroids, even though it may be very poorly known.
Note (2):
The epoch is the Julian date (TDT) ending in 00.5 nearest the date the
file was created. Thus, as the file is updated, epochs will succeed
each other at 100-day intervals on or after Julian dates ending in
50.5 (19960308, 19960616, 19960924, 19970102,...)
Note (3): the osculating elements are heliocentric, on J2000
Note (4): Planet-crossing asteroids
(Note: Because some orbits are very poor (or erroneously linked),
there may be errors in assignment of these parameter values)
The values are:
1 = Earth-crossing asteroid (ECA), according to Shoemaker et al.'s
definition (In "Asteroids", pp. 253-282, T. Gehrels, ed., The
University of Arizona Press, Tucson, 1979 ). Some ECAs are
currently Amors (q.v.). ECAs have been identified prior to May
1991. After that date, asteroids having q < 1.0167 AU have been
assumed to be ECAs. Thus, in the latter group, some may not be
ECAs, and some asteroids assumed to be Amors may be ECAs.
2 = Asteroids having perihelia less than the aphelion distance of the
Earth (1.0167 AU), but which are not ECAs.
4 = Amors (1.0167 < q < 1.3 AU) (but see also type 1).
8 = Mars crossers (1.3 < q < 1.6660 AU).
16 = Outer-planet crossers (excluding Jupiter Trojans).
n = Asteroids (excluding Mars and Jupiter Trojans) that cross both
inner- and outer-planet orbits. For example, n=24 crosses the
orbits of Mars (q < 1.6660 AU) and Jupiter (Q > 4.950 AU).
Note (5): Orbit computation.
1 = Orbits derived from uncertainly, perhaps erroneously linked
observations.
2 = Eccentricity assumed.
4 = Eccentricity and semimajor axis assumed.
8 = For numbered asteroids, omitted observations have resulted in
degradation of a so-called orbit-quality parameter (OQP, see K.
Muinonen and E. Bowell, Icarus 104, 255-279, 1993), generally by
more than 0.1. The corresponding ephemeris uncertainty has
increased by about 25% or more.
16 = OQP degrades by more than 0.1 if unsubstantiated observations
(e.g., one-night apparitions) are omitted.
32 = Orbit derived from data containing observations not in
Minor Planet Center files
64 = H is unknown; H = 14 mag assumed.
128 = Asteroid sought, but not found.
n = Sum of preceding entries. For example, n=3 pertains to an
uncertainly linked orbit for which the eccentricity was assumed.
Note (6): Asteroids observed during the course of major surveys.
Our definition includes asteroids that were observed but not
discovered during the course of a survey.
1 = Palomar-Leiden survey (PLS) asteroids.
2 = Palomar-Leiden T-2 survey asteroids.
4 = Palomar-Leiden T-3 survey asteroids.
8 = U.K. Schmidt Telescope-Caltech asteroid survey (UCAS) asteroids.
16 = Palomar-Leiden T-1 survey asteroids.
n = Asteroids observed in more than one survey. For example, n=3
denotes an asteroid observed in both the PLS and T-2 surveys.
Note (7): Minor Planet Center (MPC) critical-list numbered asteroids.
1 = Lost asteroid.
2 = Asteroids observed at only two apparitions.
3 = Asteroids observed at only three apparitions.
4 = Asteroids observed at four or more apparitions, last more than
ten years ago.
5 = Asteroids observed at four or more apparitions, only one night in
last ten years.
6 = Other poorly observed asteroids observed at four or more
apparitions.
7 = Absolute magnitude poorly known (not on MPC critical-list).
Note (8): Lowell Observatory and related discoveries
1 = Asteroids discovered by E. Bowell.
2 = Non-Bowell discoveries from Lowell search programs.
3 = Discovered jointly by E. Bowell and another person connected
with Lowell search programs.
Note (9): Rank, in decreasing importance, for our collaborative
program of astrometry using the transit circle of the
U.S. Naval Observatory Flagstaff Station.
10 = Exceptionally important, to be observed frequently. Principally
space mission targets and occultation candidates.
9 = Asteroids useful for mass determination.
8 = Asteroids for which one or two additional nights' observation
are required to satisfy orbit-update requirements. Asteroids
of type 6:7 whose ephemeris uncertainties are between 2 and 5
arcsec within the next ten years or so.
7 = Bowell unnumbered discoveries whose ephemeris uncertainties
are less than 2 arcsec within the next ten years or so. MPC
critical-list asteroids.
6 = Planet-crossers of type 6:5.
5 = Numbered asteroids whose ephemeris uncertainties are between
2 and 5 arcsec within the next ten years or so. Unnumbered
asteroids that should be numberable after one or two more
nights' observation.
Note (10): The current 1-σ ephemeris uncertainty CEU and its rate
of change dCEU indicate whether an asteroid ought to be located in an
observer's field of view. A CEU greater than all three of the peak
ephemeris uncertainties (PEU) implies that the asteroid's ephemeris
uncertainty is currently greater than at any time in the next ten
years. Such asteroids are prime targets for observation because their
orbits are subject to the greatest improvement for years to come. Note
that, because ephemeris uncertainties have been computed using 2-body
rather than n-body error propagation (see K. Muinonen and E. Bowell,
Icarus 104, 255-279, 1993), uncertainties for Earth-approaching
asteroids may have been misestimated by a factor of several.
Note (11): Peak ephemeris uncertainties generally occur
near opposition or conjunction (the latter are more prevalent for
Earth-crossing asteroids). The next PEU [parameter PEU0] usually
indicates the best time to make astrometric observations for orbit
improvement, as will the PEU over the next 10 years [parameter PEU1].
Special effort should be made to observe asteroids whose next PEUs are
the greatest during the next 10 years [i.e., parameter PEU0 exceeds
both parameters PEU1 and PEU2]. Parameter PEU2 may be used to quantify
the amount of orbital improvement that would result from observing at
or near the date of next PEU. For example, if the next PEU is 1.2D+02
arcsec, and parameter PEU2 has value 6.0D+00 arcsec, a 20-fold
ephemeris improvement (and approximately equal improvement in the
uncertainties of the orbital elements) could be made. Note that
numbered asteroids whose orbits are satisfactory have all three PEUs
less than about 2 arcsec (absolute). Consequently, numbered asteroids
whose ephemeris uncertainties, as indicated by the CEU and PEUs, at
any time exceed about 2 arcsec should be targeted for observation.
Unnumbered asteroids whose ephemeris uncertainties [as per parameter
PEU2] could be brought below about 2 arcsec, would probably then be
candidates for numbering. A parameter PEU2 PEU greater than a
parameter PEU1 PEU implies that observing at or near the date of the
next PEU [parameter PEU0] may actually cause ephemeris and orbit
degradation. Thus, there is no point in making such observations
unless they are numerous and/or of high accuracy.
Note (12): the two columns "mod" and "modDate" are added at CDS and
precises the date of the last modification of the number of
observations (columns "Nobs" and "Narc"). The column "mod" contains
an "a" for the date of addition of the asteroid, and a "*" for the
date of last change in the number of observations. Note that the
date is only approximative to about 1 week.
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History:
* The orbital elements of the Asteroids are regularly (weekly) updated
from October 1996 on from the Lowell server at ftp.lowell.edu
(End) CDS Catalogues Service 2009-May-10