Table 2.
StereoCAT fitting parameters chosen for the CME candidates.
| ϕ (°) | θ (°) | α (°) | Vcme (km s−1) | Passes at 21 R⊙ | |
|---|---|---|---|---|---|
| CME 1 | −60 | 48 | 17 | 224 | 2013/06/23 18:30 |
| CME 2 | −62 | −15 | 20 | 489 | 2013/06/24 06:01 |
| CME 3 | 14 | 14 | 27 | 391 | 2013/06/24 09:17 |
| CME 4 | 175 | −15 | 56 | 844 | 2013/06/24 07:47 |
| CME 5 | −41 | 61 | 22 | 487 | 2013/06/25 15:53 |
| CME 6 | 175 | −21 | 38 | 620 | 2013/06/25 16:48 |
Notes. The terms are as follows: ϕ(°) is the heliographic longitude; θ(°) is the heliographic latitude, both measured in the HEEQ system (Heliocentric Earth Equatorial); α(°) is the angle between the legs; Vcme (km s−1) is the CME speed propagation; and ‘Passes at 21 R⊙’ indicates the time when the CME reaches 21.5 R⊙, according to the model parameters. Bold indicates the CME event responsible for the signal seen by the spacecraft.
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