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Table 3.
Electron peak spectra results.
| Spacecraft | δ200 | δ1 | δ2 | δ3 | Eb1 (keV) | Eb2 (keV) | α | β |
|---|---|---|---|---|---|---|---|---|
| Wind | −2.81 ± 0.13 | −2.81 ± 0.13 | – | – | – | – | – | – |
| Solar Orbiter | −2.59 ± 0.07 | −1.76 ± 0.76 | −2.59 ± 0.07 | −3.19 ± 1.40 | 51 ± 12 | 458 ± 1634 | 21.21 | 141.24 |
| STEREO-A | −2.82 ± 0.13 | −2.59 ± 0.07 | −2.82 ± 0.13 | – | 94 ± 13 | – | 11.59 | – |
Notes. Parameters based on the method described by Dresing et al. (2020) and Strauss et al. (2020). Details given in the main text.
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