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Table C.3.

Orbital elements of S1and S2, expressed in EQJ2000.

S1 – S/2003 (130) 1
Observing data set
Number of observations 150
Time span (days) 22
RMS (mas) 3.53

Orbital elements EQJ2000
P (day) 5.287 ± 0.004
a (km) 1353 ± 17
e 0.09 ± 0.02
i (°) 161 ± 1
Ω (°) 179 ± 3
ω (°) 179 ± 7
tp (JD) 2456990.85 ± 0.08
(αp, δp) (°) (89, −71) (± 3, ±1)
(λp, βp) (°) (277, −87) (± 20, ±2)

S2 – S/2014 (130) 1

Observing data set
Number of observations 120
Time span (days) 22
RMS (mas) 2.39

Orbital elements EQJ2000
P (day) 1.192 ± 0.002
a (km) 501 ± 7
e 0.03 ± 0.03
i (°) 156 ± 7
Ω (°) 187 ± 10
ω (°) 235 ± 18
tp (JD) 2456990.53 ± 0.06
(αp, δp) (°) (97, −66) (± 10, ±7)
(λp, βp) (°) (165, −87) (± 113, ±4)

Notes. Orbital period P, semi-major axis a, eccentricity e, inclination i, longitude of the ascending node Ω, argument of pericentre ω, time of pericentre tp, ecliptic J2000 coordinates of the orbital pole (λp, βp), and equatorial J2000 coordinates of the orbital pole (αp, δp). The number of observations and RMS between the predicted and observed positions are also provided. Uncertainties are given at 1-σ.

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