Outer Natural Satellites Orbits Ephemerides.
Outer satellites of Jupiter
Choose type of the ephemeride:
Trigonometric series for the orbital elements (
a, e, i, ω, Ω
)
Values of the orbital elements
[
output
e⋅sin(ω), e⋅cos(ω), sin(i)⋅sin(Ω), sin(i)⋅cos(Ω)
]
Distances between the osculating orbits
Choose Satellite
J06 - Himalia
J07
J08
J09
J10
J11
J12
J13
J17
J18
J19
J20
J21
J22
J23
J24
J25
J26
J27
J28
J29
J30
J31
J32
J33
J34
J35
J36
J37
J38
J39
J40
J41
J42
J43
J44
J45
J46
J47
J48
J49
J50
S/2003 J2
S/2003 J3
S/2003 J4
S/2003 J5
S/2003 J9
S/2003 J10
S/2003 J12
S/2003 J15
S/2003 J16
S/2003 J18
S/2003 J19
S/2003 J23
of Jupiter
Choose Second Satellite (for the distances)
J07 - Elara
J08
J09
J10
J11
J12
J13
J17
J18
J19
J20
J21
J22
J23
J24
J25
J26
J27
J28
J29
J30
J31
J32
J33
J34
J35
J36
J37
J38
J39
J40
J41
J42
J43
J44
J45
J46
J47
J48
J49
J50
S/2003 J2
S/2003 J3
S/2003 J4
S/2003 J5
S/2003 J9
S/2003 J10
S/2003 J12
S/2003 J15
S/2003 J16
S/2003 J18
S/2003 J19
S/2003 J23
For the Values and Distances
Enter initial date (years)
Enter final date (years)
Enter step of dates (years)
Enter lower limits for amplutudes of
semi-major axis
Gm
eccentricity
inclination
deg.
pericenter
deg.
node
deg.
Enter upper limit of frequency
deg/year
At least
do not include short-period terms (f > n)