Table 5
Distribution of the accuracy with which fit parameters are recovered.
| 5 yr | 10 yr | |||||
|---|---|---|---|---|---|---|
| 25% | 50% | 75% | 25% | 50% | 75% | |
| P | 0.14% | 0.70% | 6.5% | 0.058% | 0.29% | 1.8% |
| υ | 3.1% | 8.0% | 18% | 2.3% | 6.0% | 14% |
| e | 0.030 | 0.077 | 0.17 | 0.025 | 0.061 | 0.14 |
| cos i | 0.031 | 0.078 | 0.17 | 0.023 | 0.051 | 0.11 |
| Ω | 2.7° | 7.3° | 25° | 1.9° | 5.2° | 16° |
| ω | 8.4° | 21° | 45° | 6.0° | 18° | 41° |
| Tp∕P | 0.015 | 0.045 | 0.16 | 0.011 | 0.032 | 0.11 |
Notes. The first column presents the orbital parameter; the other columns present the distribution of the length of its 68.3% error bars in the 5 yr mission (Cols. 2–4) and in the 10 yr mission (Cols. 5–7) as the 25% quartile, median, and 75% quartile. Relative errors are shown for quantities that vary over several orders of magnitude, namely P and υ; absolute errors for the remaining parameters. We consider Tp∕P (instead of just Tp) because it isalways contained in the [0, 1] interval.
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