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J/AJ/153/147
152
The orbits of Jupiter's irregular satellites (Brozovic+, 2017)
ReadMe+ftp
2017AJ....153..147B
Similar Catalogs
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1.
J/AJ/153/147/table2
Post-fit residual statistics
(59 rows)
meta
J/AJ/153/147/table2
2.
J/AJ/153/147/table3
Jupiter barycentric state vectors at 2010 January 1 TDB referred to the ICRF
(177 rows)
meta
J/AJ/153/147/table3
3.
J/AJ/153/147/table5
Orbital uncertainties in the plane-of-sky, in-orbit, radial, and out-of-plane directions
(157 rows)
meta
J/AJ/153/147/table5
4.
J/AJ/153/147/table6
*Planetocentric mean orbital elements in ecliptic coordinates for 59 irregular jovian satellites
(Note)
(60 rows)
meta
J/AJ/153/147/table6
5.
J/AJ/153/147/table7
Minimum and maximum values of osculating orbital elements, and their averages over 1000 yr
(59 rows)
meta
J/AJ/153/147/table7
Simple Constraint
List Of Constraints
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Constraints
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Column
Constraint
Explain
(
UCD
)
(ALL)
recno
Record number assigned by the VizieR team. Should Not be used for identification.
(
meta.record
)
(
RECORD
)
(ALL)
Sat
(char)
Satellite identifier
(
meta.id;meta.main
)
(
ID_MAIN
)
(1)
b_Time
yr
[1894/2011] Time span, lower value
(
time.interval;stat.min
)
(
ERROR
)
(1)
B_Time
yr
(n)
[2003/2016] Time span, upper value
(
time.interval;stat.max
)
(
ERROR
)
(1)
N1
[8/3257] First number of points used in orbital fit
(
meta.number
)
(
NUMBER
)
(1)
N2
(n)
[309/3251] Second number of points used in orbital fit
(
meta.number
)
(
NUMBER
)
(1)
rmsRA
arcsec
[0.118/0.656] rms of the post-fit residuals in Right Ascension
(Note 1)
(
stat.fit.residual
)
(
FIT_RESIDUAL
)
(1)
rmsDE
arcsec
[0.109/0.679] rms of the post-fit residuals in Declination
(
stat.fit.residual
)
(
FIT_RESIDUAL
)
(1)
sRA
[0.395/1.056] Reduced rms of the post-fit residuals in Right Ascension (in σ units)
(Note 1)
(
stat.fit.residual
)
(
FIT_RESIDUAL
)
(1)
sDE
[0.365/1.138] Reduced rms of the post-fit residuals in Declination (in σ units)
(
stat.fit.residual
)
(
FIT_RESIDUAL
)
(2)
Pos
km
Position of state vector
(Note 1)
(
pos.distance
)
(
PHYS_DISTANCE_TRUE
)
ALL
cols
(n)
indicates a possible blank or NULL column
(i)
indexed column
(2)
Vel
km/s
Velocity of state vector
(Note 1)
(
phys.veloc;pos.barycenter
)
(
VELOC_BARYCENTER
)
(3)
Year
(char)
yr
Year center
(Note 1)
(
time
)
(
TIME_DATE
)
(3)
P-S
arcsec
(n)
[0.02/1500] Plane-of-sky uncertainty
(Note 2)
(
stat.error
)
(
ERROR
)
(3)
In-O
km
(n)
[37/5304000] In-orbit uncertainty
(Note 3)
(
stat.error
)
(
ERROR
)
(3)
R
km
(n)
[15/871400] Radial uncertainty
(Note 3)
(
stat.error
)
(
ERROR
)
(3)
Out-P
km
(n)
[24/36700] Out-of-plane uncertainty
(Note 3)
(
stat.error
)
(
ERROR
)
(4)
Group
(char)
[prj] Object group
(Note 1)
(
src.class
)
(
CLASS_MISC
)
(4)
a
km
Semimajor axis
(
phys.angSize.smajAxis;src.orbital
)
(
ORBIT_SIZE_SMAJ
)
(4)
e
[0.045/0.491] Eccentricity
(
src.orbital.eccentricity
)
(
ORBIT_ECCENTRICITY
)
(4)
Inc
deg
[16.27/168.79] Inclination
(
src.orbital.inclination
)
(
POS_INCLIN_LOS
)
(4)
lambda
deg
[11.2/359.01] Mean longitude λ
(
src.orbital
)
(
ORBIT_PHASE-ANGLE
)
(4)
omega
deg
[3.95/349.72] Longitude of periapsis ω
(
src.orbital.periastron
)
(
ORBIT_P-ASTRON_ARG
)
(4)
Omega
deg
[1.32/358.58] Longitude of the ascending node Ω
(
src.orbital.node
)
(
ORBIT_ASC-NODE
)
ALL
cols
(n)
indicates a possible blank or NULL column
(i)
indexed column
(4)
dl/dt
deg/d
[0.0831/2.7688] Mean longitude rate dλ/dt
(
src.orbital
)
(
ORBIT_PHASE-ANGLE
)
(4)
Per
d
[130.02/4332.59] Orbital period P
λ
(
time.period
)
(
TIME_PERIOD
)
(4)
do/dt
deg/yr
[-3.1915/1.5737] Rate of apsidal precession dω/dt
(
arith.rate;pos.precess
)
(
POS_PRECESSION
)
(4)
dO/dt
deg/yr
[-3.191/5.7262] Rate of nodal precession dΩ/dt
(
arith.rate;pos.precess
)
(
POS_PRECESSION
)
(4)
nu
(n)
[-1/1.23] Ratio of apsidal and nodal precession rates ν
(Note 2)
(
pos.precess
)
(
POS_PRECESSION
)
(4)
l_Class
(char)
[~] Limit flag on Class
(
meta.code.error
)
(
CODE_LIMIT
)
(4)
Class
(char)
Classification based on a value of ν
(Note 3)
(
src.class
)
(
CLASS_MISC
)
(5)
b_aosc
km
Osculating semimajor axis minimum value
(
phys.size.smajAxis;stat.min
)
(
ERROR
)
(5)
aoscavg
km
Osculating semimajor axis mean value
(
phys.angSize.smajAxis;src.orbital
)
(
ORBIT_SIZE_SMAJ
)
(5)
B_aosc
km
Osculating semimajor axis maximum value
(
phys.size.smajAxis;stat.max
)
(
ERROR
)
(5)
b_eosc
[0/0.29] Osculating eccentricity minimum value
(
src.orbital.eccentricity;stat.min
)
(
ERROR
)
(5)
eoscavg
[0.104/0.485] Osculating eccentricity mean value
(
src.orbital.eccentricity
)
(
ORBIT_ECCENTRICITY
)
(5)
B_eosc
[0.156/0.701] Osculating eccentricity maximum value
(
src.orbital.eccentricity;stat.max
)
(
ERROR
)
ALL
cols
(n)
indicates a possible blank or NULL column
(i)
indexed column
(5)
b_iosc
deg
[25.5/161] Osculating inclination minimum value
(
src.orbital.inclination;stat.min
)
(
ERROR
)
(5)
ioscavg
deg
[27.7/164.8] Osculating inclination mean value
(
src.orbital.inclination
)
(
POS_INCLIN_LOS
)
(5)
B_iosc
deg
[29.7/168.5] Osculating inclination maximum value
(
src.orbital.inclination;stat.max
)
(
ERROR
)
ALL
cols
(n)
indicates a possible blank or NULL column
(i)
indexed column
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