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Fig. 5

image

Mass of the primary as a function of the secondary mass, derived by fixing the mass function to the value of Table 2. Curves were calculated for each orbital inclination from 90° to 10° in steps of 10°. Dotted lines indicate the primary mass, M1 = 33 M, and the minimum possible secondary mass, M2 = 1.61 M, for reference.

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