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Table 3
Orbital solution for IGR J17252–3616.
| Units | Free Porb | Fixed Porb | RXTE Epoch 3 | |
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HJD | 53 761.73144 | 53 761.73142 | 53 761.73126 |
|
s | 413.889 ± 0.004 | 413.889 ± 0.005 | 413.894 ± 0.002 |
| Ṗ XTE | μs s-1 | –0.010 ± 0.002 | –0.010 ± 0.003 | –0.0106 ± 0.0001 |
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HJD | 53 978.7494 | 53 978.7495 | – |
|
s | 413.86 ± 0.04 | 413.84 ± 0.04 | – |
| Ṗ XMM | μs s-1 | 0.98 ± 0.04 | 1.01 ± 0.03 | – |
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| αxsini | lt-s | 102 ± 8 | 101 ± 2 | 101 ± 4 |
| P orb | d | 9.76 ± 0.02 | 9.742 (fixed) | 9.78 ± 0.04 |
| T 90 | HJD | 53 761.62 ± 0.1 | 53 761.69 ± 0.1 | 53 761.60 ± 0.09 |
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1.5 (30) | 1.65 (31) | 1.45 (28) | |
Notes. The errors have been calculated at 90% confidence level. The errors in the arrival times t0 are 0.00001 and 0.0001 days for RXTE and XMM, respectively. The last column shows the result from Thompson et al. (2007) for comparison.
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