Table E.1.
EC model fit parameters in RTN coordinates
| s/c | Longitude | Tilt | Rotation | Ellipse ratio | Cross-section | Distance | χ2 | Chirality | Solar wind |
|---|---|---|---|---|---|---|---|---|---|
| ϕ (deg) | θ (deg) | ξ (deg) | δ (-) | R (au) | Y0 (au) | (km s−1) | |||
| (1) | (2) | (3) | (4) | (5) | (6) | (7) | (8) | (9) | (10) |
| Wind MC | 157 | 17 | 7 | 0.70 | 0.10 | 0.075 | 0.15 | Positive | 593 |
| SolO MC | 214 | -10 | 70 | 0.79 | 0.051 | -0.026 | 0.27 | Negative | 460 |
Notes. Column 1: Spacecraft. Column 2: MFR axis longitude (ϕ=[0...360]°). Column 3: inclination of the flux rope with respect to the equatorial plane (θ=[-90...+90]°). Column 4: MFR rotation about its central axis (ξ=[0...180]°). Column 5: MFR distortion (ratio between major and minor ellipse axis, δ=[0...1]). Column 6: MFR size. Column 7: distance from the spacecraft trajectory to the MFR axis (negative value means that the spacecraft is crossing the upper part of the structure). Column 8: goodness of the fitting (χ2=[0...1]). Column 9: MFR handedness. Column 10: average solar wind speed used for the fitting.
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