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Table 4
K2-106 system parameters.
| K2-106 | |
|
|
|
| M∗[M⊙] | 0.945 ± 0.063 |
| R∗[R⊙] | 0.869 ± 0.088 |
| Teff[K] | 5470 ± 30 |
| Linear limb-darkening coefficient u1 |
|
| Quadratic limb-darkening coefficient u2 |
|
| q 1 |
|
| q 2 |
|
|
|
|
| K2-106 b | |
|
|
|
| T0 [days] | 2457394.0114 ± 0.0010 |
| Period [days] |
|
| Impact parameter b |
|
| a / R ∗ |
|
| R p / R ∗ |
|
| Radial velocity semi-amplitude K[m s-1] | 6.67 ± 0.69 |
| Orbital eccentricity e | 0.0 (fixed) |
|
0.0 (fixed) |
|
0.0 (fixed) |
| Inclination i[deg] |
|
| Orbital semi-major axis a [AU] | 0.0116 ± 0.0013 |
| Mp[M⊕] |
|
| Rp[R⊕] | 1.52 ± 0.16 |
| ρp[g cm-3] |
|
| gp[cm s-2] |
|
 [K] |
|
| τ14 [h] |
|
| τ12 = τ34 [h] |
|
|
|
|
| K2-106 c | |
|
|
|
| T0 [days] |
|
| Period [days] |
|
| Impact parameter b |
|
| a / R ∗ |
|
| R p / R ∗ |
|
| Radial velocity semi-amplitude K[m s-1] |
|
| Orbital eccentricity e |
|
| ω |
|
|
|
0.01 ± 0.25 |
|
|
|
| Inclination i[deg] |
|
| Orbital semi-major axis a [AU] |
|
| Mp[M⊕] |
|
| Rp[R⊕] |
|
| ρp[g cm-3] |
|
| gp[cm s-2] |
|
| Teq [K] |
|
| τ14 [h] |
|
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