Table 1.
Observed times of the shock, leading and trailing edges of the magnetic ejecta at multiple spacecraft.
| Shock | ME LE | ME TE | Sheath [h] | ME [h] | VB [km s−1] | |
|---|---|---|---|---|---|---|
| Bepi | 2021-09-25T01:46:00 | 2021-09-25T09:35:00 | 2021-09-25T18:50:00 | 7.8 | 9.25 | 401.9 |
| Solar Orbiter | 2021-09-25T18:25:00 | 2021-09-26T04:37:00 | 2021-09-27T00:00:00 | 10.2 | 19.4 | 407.9 |
| PSP | 2021-09-26T08:50:00 | 2021-09-26T23:04:00 | 2021-09-27T12:40:00 | 14.2 | 13.6 | 423.5 |
| STA | 2021-09-27T01:51:00 | 2021-09-27T15:35:00 | 2021-09-28T04:31:00 | 13.7 | 12.9 | 426.4 |
| ACE | 2021-09-27T04:16:00 | 2021-09-27T04:16:00 | 2021-09-28T09:25:00 | 29.2 | N/A | 428.7 |
Notes. The first column lists the spacecraft at which the CME was observed in situ. The second to the fourth columns show the arrival times in (UT) of the shock, ME LE, and ME TE at the observing spacecraft. The last three columns show the duration of the sheath and magnetic cloud in hours and the ballistic propagation speed in km s−1. The ballistic speed is calculated with VB = (spacecraft location-1 R⊙)/(Shock-eruption time).
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