Open Access

Table A.2

Table containing information regarding the dual-spacecraft bow shock crossings where the spacecraft were located in different E hemispheres.

Event number d+E [RM] dE [RM] d+E-dE [RM] sc+ E Δt [Min] MA Pdyn [nPa] EUV [mWm−2]
26 0.017 -0.095 0.112 mav 4.0 1.8 0.92 19.7
30 0.238 0.137 0.101 mav 18.7 1.3 2.47 19.6
38 -0.085 0.063 -0.147 mex 18.0 2.4 0.90 27.2
41 0.049 0.173 -0.124 mex 1.9 6.4 1.13 27.4
51 0.0855 0.109 -0.023 mex 4.9 2.7 0.80 27.4
71 0.107 0.092 0.014 mex 11.8 0.9 0.20 27.7
74 0.220 0.175 0.044 mav 18.5 1.9 1.52 27.7
91 0.020 0.173 -0.153 mav 4.5 4.2 0.46 27.9
144 0.272 0.044 0.228 mex 9.5 4.1 0.45 26.9
153 0.281 0.335 -0.053 mex 40.8 0.4 0.50 26.6
176 0.104 0.031 0.072 mav 15.0 3.2 0.36 26.3

Mean 0.119 0.112 0.006 16.3

1σ 0.119 0.109 0.121

Notes. The first column shows event ID. The second and third columns show the distance from the bow shock model to the observed bow shock crossing by on the + E and −E hemisphere, respectively. The fourth column shows the difference between these two distances. The fifth column shows which spacecraft crossed the bow shock in the + E hemisphere. The sixth column shows the time difference between the crossings. The seventh to ninth column shows upstream values of Alfvénic Mach number, dynamic pressure, and solar EUV, respectively. At the bottom two rows the mean and one standard deviation for the distances, and for the difference, is given.

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