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Breaking the symmetry: X-ray polarization from a spreading layer on a tilted weakly magnetized neutron star

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Abstract

When modeling the emission from an X-ray binary system, we often assume that the rotational axis of the compact object is aligned with that of the binary system. While often considered irrelevant for spectroscopic observations, the orientation of the binary system is crucial for polarimetric properties. With the recent advent of X-ray polarimetric observations enabled by the Imaging X-ray Polarimetry Explorer (IXPE), indications of a possible misalignment of the neutron star rotational axis with respect to the binary axis have been reported. Following these indications, we present an analytical model for the polarimetric properties of emission arising from a spreading layer on an inclined weakly magnetized neutron star (WMNS). We discuss the expected polarimetric properties and study the impact of geometrical parameters of the system on the polarization of WMNS emission. We compare our results with those for aligned systems. Finally, we discuss applications of the model to recent and upcoming X-ray polarimetric observations with IXPE and mention the suggestions for further development of the model.

Introduction

In an X-ray binary with a weakly magnetized neutron star (WMNS), the accretion flow is barely affected by the magnetosphere of the neutron star (NS) and is instead shaped by gravity. Once the companion star fills its Roche lobe, matter from the outer layers of the companion star is transferred towards the NS. The matter transferred through the inner Lagrangian point carries a high specific angular momentum; it circulates around the NS, forming an accretion disk [40].

In WMNS systems, the mass accretion rate is so high that the accretion disk can push the magnetosphere towards the NS surface or even burying it beneath the NS surface. Consequently, the accretion disk is either mildly affected by the magnetosphere or reaches the NS surface unaffected by the magnetic field; in either scenario, matter accretes onto the equatorial region of the NS rather than onto the magnetic field poles as in pulsars. As the accretion disk reaches the NS surface, the matter is forced to decelerate rapidly from near-Keplerian velocities in the accretion disk to the rotational velocity of the NS surface before settling onto the NS. A so-called boundary layer (BL; see, e.g., Shakura & Sunyaev 1988) is formed. The accreted matter can subsequently spread over the NS surface, forming a spreading layer (SL, Inogamov & Sunyaev 1999).1

The spectrum of WMNS systems is traditionally decomposed into two main components: the softer disk emission and the harder emission from the BL/SL. Additional spectral features include reflection of the harder component from the disk and scattering of the emission in the wind above the disk. With spectroscopy alone, the disk and BL/SL components are often hard to distinguish. Timing analysis helps distinguish these components, since BL/SL emission is expected to vary on much faster timescales. For instance, quasi-periodic oscillations (QPOs) have been shown to be associated with the BL/SL region (Galfon et al. 2003; Revnivtsev & Gilfanov 2006). However, timing cannot determine the exact geometry of the accretion flow or distinguish between the BL and SL configurations.

Polarimetry holds promise to investigate the geometry of binary systems. With the launch of the Imaging X-ray Polarimetry Explorer (IXPE); Weisskopf et al. 2022) in December 2021, it became possible, for the first time, to measure with high precision the polarization degree (PD) and polarization angle (PA) of X-ray emission. In addition to providing information on the geometrical configuration of the system, polarimetric properties carry information about the processes affecting the emission as it travels from the source to the observer, since X-ray emission becomes polarized through scattering, reflection, or interaction with the magnetic field. In recent years, more than twenty WMNS systems have been observed with IXPE, and observations of many of these systems have provided constraints on the source geometry.

Since the early stages of X-ray astronomy, various theoretical models for the expected polarized emission of binary systems have been developed in preparation for X-ray polarimetric observations. For instance, the polarimetric properties of accretion disks were studied in Rees [38] based on pioneering work of Chandrasekhar [4] and Sobolev [42], under the assumption of electron-scattering-dominated disk atmospheres. Relativistic effects were later incorporated into the model by, e.g., Connors et al. [6], Dovčiak et al. [11], and Loktev et al. [26]. Currently, for linear polarization in the IXPEIXPE energy range, the expected PD is 2% for moderate inclination, rising to 6% for i=80∘i = 80^\circ [26]. Polarization is expected to be aligned with the accretion disk plane.

For the BL/SL, polarimetric expectations strongly depend on the geometry of the region. Both pioneering analytical works [44, 24] and modern numerical simulations, e.g., Gnarini et al. (2022), predict that emission arising from a BL configuration of the accretion flow is polarized in the plane of the accretion disk, whereas for the SL configuration, the emission is expected to be polarized perpendicular to the disk plane. In recent analytical modeling, Bobrikova et al. [3] calculated that the PD of the SL is not expected to exceed 1.5% and that the emission is polarized in the plane perpendicular to the accretion disk, with minor variations depending on the energy and geometrical configuration of the system. Similar conclusions are presented in Farinelli et al. [13].

Both scattering in the wind [31] and reflection from the accretion disk [24, 29, 34] are expected to boost the total polarization of the WMNS emission. However, the contributions of reflection component to the total flux are usually small, and the scattered fraction is low for the systems observed from low and medium inclinations [31], so the general expected PD of WMNS systems remains relatively low.

However, recent IXPEIXPE observations have shown that for many sources the observed PD values significantly exceed theoretical expectations (see, e.g., Ursini et al. 2024; Di Marco 2025; Gnarini et al. 2025, for reviews). In several cases, at higher energies, where the Comptonized component is expected to dominate the flux, the PD exceeded 10%. Among possible explanations for the high PD, scattering in the wind and reflection from the disk are usually mentioned (see, among many others, Gnarini et al. 2025); however, not all the systems are known to have strong winds or to show signs of reflection. For instance, GX 5−1 is known for a lack of reflection features [18] and does not show signs of a strong wind in X-ray spectroscopy, yet the observed PD exceeds 4% at higher energies [12]. One possible explanation for the unexpectedly high PD in these systems is a breaking of the axial symmetry.

Another known issue is the PA of the continuum components: although theoretically the PA of the Comptonized component is expected to be aligned with or orthogonal to that of the disk, for several sources, a PA difference of about 60° has been observed. Notably, the young X-ray binary Cir X-1 was one such source, and in this source, a misalignment between the rotational axis of the NS and the binary axis was suggested as a possible explanation [36], since hints of misalignment such as precession of the accretion disk and twisted jets had already been observed in this system [7, 8].

Here, we introduce an analytical model of polarized SL emission from a misaligned NS. In Sect. 2 we present the model, describing the physical properties of the SL emission, its propagation, and the geometrical configuration of the system. In Sect. 3 we present the results of our study of the impact of various system parameters on the observed emission. We discuss the application of our model to previous IXPEIXPE observations in Sect. 4. Finally, we conclude in Sect. 5.

Model setup

The geometry of the system is shown in Figure 1. We consider a spherical NS of radius RR and mass MM with a SL centered at the NS equator and extending between the co-latitudes of the SL edges, θmin⁡\theta_{\min} and θmax⁡=180∘−θmin⁡\theta_{\max} = 180^\circ- \theta_{\min}. The matter in the SL flows counterclockwise with the equatorial velocity βeq\beta_{\rm eq}; the velocity decreases towards the poles as described in Eq. (A.4). The SL emission is assumed to be a (modified) blackbody at the constant effective temperature TeffT_{\rm eff} and is modeled as a semi-infinite electron-scattering-dominated plane-parallel slab.

Geometry of the problem

Figure 1. Geometry of the problem. The rotational axis of the NS ω\omega is misaligned relative to the rotational axis of the binary system (zz) by an angle η\eta. The rotational axis of the NS forms the azimuthal angle Φ\Phi (marked with a purple solid line) with the direction to the observer (k^\hat{k}). The inclinations of the binary system, ii, and of the NS, i∗i_*, are indicated by black dotted and brown dashed lines, respectively. The SL is shown in dark purple and is confined between co-latitudes θmin⁡\theta_{\min} (marked with a blue dashed line) and θmax⁡=180∘−θmin⁡\theta_{\max} = 180^\circ- \theta_{\min}. The accretion disk lies in the xyxy plane; it is omitted from the sketch for clarity.

We assume that the rotation axis of the binary system is aligned with the zz-coordinate axis, and the accretion disk lies in the xyxy-coordinate plane. The coordinates are chosen so that the unit vector in the direction of the observer k^\hat{k} lies in the xzxz plane and makes an angle ii with the binary rotation axis, giving

k^=(sin⁡i,0,cos⁡i).(1)\hat{k} = (\sin i, 0, \cos i). \tag*{(1)}

We assume that the NS rotational axis ω^\hat{\omega} is misaligned with respect to the rotational axis of the binary system by an angle η\eta. In the binary plane, the NS rotation axis forms an azimuthal angle Φ\Phi with the direction to the observer k^\hat{k}. In Figure 1, η\eta is measured from the positive zz-axis, while Φ\Phi is measured in the xyxy-plane from the positive xx-axis. Hence, the NS rotational axis is defined as follows:

ω^=(sin⁡ηcos⁡Φ,sin⁡ηsin⁡Φ,cos⁡η).(2)\hat{\omega} = (\sin\eta\cos\Phi, \sin\eta\sin\Phi, \cos\eta). \tag*{(2)}

The NS inclination i∗i_*, defined as the angle between the direction to the observer and the NS rotational axis ω^\hat{\omega}, is given by

cos⁡i∗=k^⋅ω^=cos⁡icos⁡η+sin⁡isin⁡ηcos⁡Φ.(3)\cos i_* = \hat{k} \cdot\hat{\omega} = \cos i \cos\eta+ \sin i \sin\eta\cos\Phi. \tag*{(3)}

To relate the current model to the axisymmetric case presented in B25, where the NS rotation axis was aligned with the orbital axis, we move to the coordinate system associated with the NS. We then define all the necessary vectors in that new coordinate system, which we refer to as the “NS frame”, and denote their coordinates with the subscript *. Here, z^∗\hat{z}_* is aligned with the NS rotational axis ω^=(0,0,1)∗\hat{\omega}=(0,0,1)_* and we define the coordinate axes as follows:

x^∗=y^∗×ω^=(k^−ω^cos⁡i∗)/sin⁡i∗,\hat{x}_*=\hat{y}_*\times\hat{\omega}=(\hat{k}-\hat{\omega}\cos i_*)/\sin i_*,
y^∗=ω^×k^/sin⁡i∗,\hat{y}_*=\hat{\omega}\times\hat{k}/\sin i_*,
z^∗=ω^.(4)\hat{z}_*=\hat{\omega}. \tag*{(4)}

The direction to the observer in this system is

k^=(sin⁡i∗,0,cos⁡i∗)∗.(5)\hat{k}=(\sin i_*,0,\cos i_*)_*. \tag*{(5)}

Introducing the co-latitude θ\theta and the azimuthal angle ϕ\phi, which specify a point on the NS surface in that coordinate system, we can define the normal to the surface element:

n^=(sin⁡θcos⁡ϕ,sin⁡θsin⁡ϕ,cos⁡θ)∗.(6)\hat{n}=(\sin\theta\cos\phi,\sin\theta\sin\phi,\cos\theta)_*. \tag*{(6)}

This geometry is used to calculate the polarized emission from the SL on an aligned NS using the formalism presented in Suleimanov et al. [43] and B25. For completeness, we provide the necessary formulae in Appendix A. We assume that the spectrum of the local emission can be described by a diluted blackbody

IE′′(α′)=aes(α′)1fc4BE′(fcTeff),(7)I'_{E'}(\alpha')=a_{\rm es}(\alpha')\frac{1}{f_{\rm c}^{4}}B_{E'}(f_{\rm c}T_{\rm eff}), \tag*{(7)}

where BE′B_{E'} is the Planck function, fcf_{\rm c} is the color correction factor, and aes(α′)=0.421+0.868cos⁡α′a_{\rm es}(\alpha')=0.421+0.868\cos\alpha' is an approximation to the angular distribution of radiation intensity from a semi-infinite, electron-scattering-dominated atmosphere ([5]) as a function of the zenith angle α′\alpha' in the local comoving frame of the gas. The polarized flux (Stokes vector) observed from an SL surface element dS\mathrm{d}S is given by

dF(E)=(dFI(E)dFQ(E)dFU(E))=dFE(1P(α′)cos⁡2χP(α′)sin⁡2χ),(8)\mathrm{d}F(E)= \begin{pmatrix} \mathrm{d}F_I(E)\\ \mathrm{d}F_Q(E)\\ \mathrm{d}F_U(E) \end{pmatrix} =\mathrm{d}F_E \begin{pmatrix} 1\\ P(\alpha')\cos2\chi\\ P(\alpha')\sin2\chi \end{pmatrix}, \tag*{(8)}

where PP is the PD at the zenith angle α′\alpha', calculated using the approximation ([4]) for a semi-infinite electron-scattering-dominated atmosphere. The PA χ\chi is calculated using the formula derived in Poutanen [32] that accounts for corrections caused by the relativistic motion of the SL matter and light bending in the Schwarzschild metric.

The misalignment must be included in the PA calculation. The PA is measured counterclockwise with respect to the orbital axis as χtot=χ+χm\chi_{\rm tot}=\chi+\chi_{\rm m}, where the angle χm\chi_{\rm m} is the position angle of the NS rotational axis measured eastward (i.e. counterclockwise) from the projection of the orbital axis onto the sky. To compute χm\chi_{\rm m}, we introduce the polarization basis related to the orbital coordinate system:

e^x z=z^−k^cos⁡isin⁡i=(−cos⁡i,0,sin⁡i),(9)\hat{e}^{\,z}_{x}=\frac{\hat{z}-\hat{k}\cos i}{\sin i}=(-\cos i,0,\sin i), \tag*{(9)}
e^y z=k^×z^sin⁡i=(0,−1,0).(10)\hat{e}^{\,z}_{y}=\frac{\hat{k}\times\hat{z}}{\sin i}=(0,-1,0). \tag*{(10)}

The polarization basis related to the coordinate system of the misaligned NS is similarly defined as

e^x ∗=ω^−k^cos⁡i∗sin⁡i∗=1sin⁡i∗(sin⁡ηcos⁡Φ−sin⁡icos⁡i∗sin⁡ηsin⁡Φcos⁡η−cos⁡icos⁡i∗),(11)\hat{e}^{\,*}_{x}=\frac{\hat{\omega}-\hat{k}\cos i_*}{\sin i_*} =\frac{1}{\sin i_*} \begin{pmatrix} \sin\eta\cos\Phi-\sin i\cos i_*\\ \sin\eta\sin\Phi\\ \cos\eta-\cos i\cos i_* \end{pmatrix}, \tag*{(11)}
e^y ∗=k^×ω^sin⁡i∗.(12)\hat{e}^{\,*}_{y}=\frac{\hat{k}\times\hat{\omega}}{\sin i_*}. \tag*{(12)}

Then, we calculate χm\chi_{\rm m} using

cos⁡χm=e^x ∗⋅e^x z=cos⁡ηsin⁡i−sin⁡ηcos⁡icos⁡Φsin⁡i∗,(13)\cos\chi_{\rm m}=\hat{e}^{\,*}_{x}\cdot\hat{e}^{\,z}_{x} =\frac{\cos\eta\sin i-\sin\eta\cos i\cos\Phi}{\sin i_*}, \tag*{(13)}
sin⁡χm=e^x ∗⋅e^y z=−sin⁡ηsin⁡Φsin⁡i∗,\sin\chi_{\rm m}=\hat{e}^{\,*}_{x}\cdot\hat{e}^{\,z}_{y} =-\frac{\sin\eta\sin\Phi}{\sin i_*},

or

tan⁡χm=sin⁡ηsin⁡Φsin⁡ηcos⁡icos⁡Φ−cos⁡ηsin⁡i.(14)\tan\chi_{\rm m}=\frac{\sin\eta\sin\Phi}{\sin\eta\cos i\cos\Phi-\cos\eta\sin i}. \tag*{(14)}

This expression is equivalent to the formula for the polarization angle in the rotating vector model for pulsars ([35, 30, 32]).

Once the Stokes flux observed from a surface element is obtained, we can then integrate over the whole SL. To account for light bending, we introduce the visibility condition for the surface element cos⁡α>0\cos\alpha>0, as in Suleimanov et al. [43] (see Appendix A). The misalignment of the NS rotational axis with the accretion disk axis requires one more visibility condition. The observer cannot see the parts of the NS covered by the accretion disk, which is mathematically expressed as inequality n^⋅z^>0\hat{n}\cdot\hat{z}>0. Since n^\hat{n} is defined in the coordinate system associated with the NS, we need z^\hat{z} in the same coordinate system:

z^=(e^x ∗⋅z^,e^y ∗⋅z^,e^z ∗⋅z^)∗=((cos⁡i−cos⁡ηcos⁡i∗)/sin⁡i∗−sin⁡isin⁡ηsin⁡Φ/sin⁡i∗cos⁡η)∗.(15)\hat{z}=(\hat{e}^{\,*}_{x}\cdot\hat{z},\hat{e}^{\,*}_{y}\cdot\hat{z},\hat{e}^{\,*}_{z}\cdot\hat{z})_*= \begin{pmatrix} (\cos i-\cos\eta\cos i_*)/\sin i_*\\ -\sin i\sin\eta\sin\Phi/\sin i_*\\ \cos\eta \end{pmatrix}_*. \tag*{(15)}

The second visibility condition n^⋅z^>0\hat{n}\cdot\hat{z}>0 then takes the form

cos⁡ηcos⁡θ+sin⁡ηsin⁡θcos⁡(Φ∗−ϕ)>0,(16)\cos\eta\cos\theta+\sin\eta\sin\theta\cos(\Phi_*-\phi)>0, \tag*{(16)}

where Φ∗\Phi_* is the azimuth of the orbital angular momentum vector in the NS frame and

cos⁡Φ∗=(sin⁡ηcos⁡i−cos⁡ηsin⁡icos⁡Φ)/sin⁡i∗,\cos\Phi_*=(\sin\eta\cos i-\cos\eta\sin i\cos\Phi)/\sin i_*,
sin⁡Φ∗=−sin⁡isin⁡Φ/sin⁡i∗.(17)\sin\Phi_*=-\sin i\sin\Phi/\sin i_*. \tag*{(17)}

Thus, for θ<π/2−η\theta<\pi/2-\eta, an element is visible for any ϕ\phi, whereas for θ>π/2+η\theta>\pi/2+\eta it is invisible. In the intermediate regime, π/2−η<θ<π/2+η\pi/2-\eta<\theta<\pi/2+\eta, the visibility condition reads cos⁡(Φ∗−ϕ)>−cot⁡θcot⁡η\cos(\Phi_*-\phi)>-\cot\theta\cot\eta, which is equivalent to ∣Φ∗−ϕ∣<ϕ0=π−arccos⁡(cot⁡θcot⁡η)|\Phi_*-\phi|<\phi_0=\pi-\arccos(\cot\theta\cot\eta).

The total polarized flux from the SL is then calculated as follows:

F(E)=(FI(E)FQ(E)FU(E))=R2D2∬Scos⁡α D (δ1−u)3×IE′′(α′,θ)(1P(α′)cos⁡2χtotP(α′)sin⁡2χtot) dcos⁡θ dϕ,(18)\begin{aligned} F(E)= \begin{pmatrix} F_I(E)\\ F_Q(E)\\ F_U(E) \end{pmatrix} =\frac{R^2}{D^2}\iint_S\cos\alpha\,\mathcal{D}\,(\delta\sqrt{1-u})^3 \\ &\times I'_{E'}(\alpha',\theta) \begin{pmatrix} 1\\ P(\alpha')\cos2\chi_{\rm tot}\\ P(\alpha')\sin2\chi_{\rm tot} \end{pmatrix} \,\mathrm{d}\cos\theta\,\mathrm{d}\phi, \tag*{(18)} \end{aligned}

where SS is the visible NS surface defined by the conditions cos⁡α>0\cos\alpha>0 and n^⋅z^>0\hat{n}\cdot\hat{z}>0. Here u=RS/Ru=R_{\rm S}/R is the NS compactness, RS=2GM/c2R_{\rm S}=2GM/c^2 is the Schwarzschild radius, D\mathcal{D} is the lensing factor, IE′I'_E is the intensity of escaping radiation in the comoving frame, and DD is the distance to the source. Finally, we obtain the polarimetric properties of the SL emission:

Pobs=FQ2+FU2FI(19)P_{\mathrm{obs}} = \frac{\sqrt{F_Q^2+F_U^2}}{F_I} \tag*{(19)}

and

cos⁡(2χobs)=FQPobsFI,sin⁡(2χobs)=FUPobsFI.(20)\cos(2\chi_{\mathrm{obs}}) = \frac{F_Q}{P_{\mathrm{obs}}F_I},\qquad\sin(2\chi_{\mathrm{obs}}) = \frac{F_U}{P_{\mathrm{obs}}F_I}. \tag*{(20)}

Results

We applied the formalism developed in Sect. 2 to study the effects of the misalignment in the system on the observed spectral and polarimetric properties. We use dimensionless variables, such as the photon energy:

x=EfckBTeff,(21)x = \frac{E}{f_{\mathrm{c}} k_{\mathrm{B}} T_{\mathrm{eff}},} \tag*{(21)}

where kBk_{\mathrm{B}} is the Boltzmann constant. We scaled the observed polarized flux given by (18) to the typical flux at the NS surface σSBTeff4\sigma_{\mathrm{SB}}T_{\mathrm{eff}}^4 and the ratio of the distance squared to the emitting area, to introduce the dimensionless luminosity (Stokes vector):

xlx=D2ΔR2EFEσSBTeff4=15π5∬Scos⁡α D(δ1−u)4aes(α′)x′4ex′−1(1P(α′)cos⁡2χtotP(α′)sin⁡2χtot) dcos⁡θ dϕ,(22)x\boldsymbol{l}_x = \frac{D^2}{\Delta R^2}\frac{E F_E}{\sigma_{\mathrm{SB}}T_{\mathrm{eff}}^4} = \frac{15}{\pi^5}\iint_S \cos\alpha\,\mathcal{D}\left(\delta\sqrt{1-u}\right)^4 a_{\mathrm{es}}(\alpha') \frac{x'^{4}}{e^{x'}-1} \begin{pmatrix} 1\\ P(\alpha')\cos2\chi_{\mathrm{tot}}\\ P(\alpha')\sin2\chi_{\mathrm{tot}} \end{pmatrix} \,\mathrm{d}\cos\theta\,\mathrm{d}\phi, \tag*{(22)}

where Δ\Delta is the fraction of the NS surface covered by the SL and x′=x/(δ1−u)x'=x/(\delta\sqrt{1-u}) is the dimensionless photon energy in the comoving frame (see Appendix A for details).

The results are sensitive to several parameters: the azimuthal angle Φ\Phi, the obliquity angle η\eta, the orbital inclination ii, the co-latitude of the SL edge θmin⁡\theta_{\min}, the dimensionless equatorial velocity βeq\beta_{\mathrm{eq}} (see Appendix A), and the photon energy xx. The parameter combinations used in the simulations presented in this section are listed in Table 1.

FigureΦ\Phi (deg)η\eta (deg)ii (deg)θmin⁡\theta_{\min} (deg)
Figure 3 (a)0v7560
Figure 3 (b)45v7560
Figure 3 (c)90v7560
Figure 4 (a)4515v75
Figure 4 (b)451575v
Figure 4 (c)v157575
Figure 5 (a)−−3090−η90-\eta
Figure 5 (b)−−5090−η90-\eta
Figure 5 (c)−−7090−η90-\eta
Figure 6 (a)−15−75
Figure 6 (b)−30−60

Table 1. List of parameters used in the simulations presented in this section.

Notes. Parameters varied along the plot axes are indicated by a “−” sign. The letter “v” indicates that multiple values of the parameter are used and specified in the corresponding plot legend. The equatorial velocity is fixed at βeq=0.35\beta_{\mathrm{eq}} = 0.35 for all studies presented in this section. The energy is fixed at E=5E = 5 keV for Figs. 5 and 6.

In Figure 2, a sketch of a SL on the surface of a misaligned WMNS with compactness u=0.34u = 0.34 is shown. The main regions of the SL are marked in different colors. These regions make significantly different contributions to both the luminosity and the polarimetric properties of the SL emission. Regarding the luminosity, Zone C accounts for the majority of the emission, Zone A contributes at higher energies, Zone B contributes at lower energies, and Zone D is only visible in some cases. For a plane-parallel slab, the polarimetric properties depend on the angle between the slab surface normal and the direction to the observer: the larger this angle, the larger the PD. This means that Zones A (approaching flow on the flank of the SL) and B (receding flow on the other flank of the SL) emit more strongly polarized light in the direction of the observer than Zone C (main body of the SL), whereas emission from Zone C is mostly unpolarized. Zone D (back of the SL) has a PD similar to those of Zones A and B, although the PA is different: since the emission from a plane-parallel slab is polarized in the plane of the slab surface, the PA of the emission from Zone D is almost orthogonal to those of Zones A and B.

Sketch of a spreading layer on the surface of a neutron star

Figure 2. A sketch of a SL on the surface of a NS with compactness u=0.34u = 0.34 as seen by a distant observer. The matter in the SL flows counterclockwise. The main regions of the SL are shown in different colors: red (zone A) is the flank of the SL with approaching flow; blue (zone B) is the flank of the SL with receding flow; green (zone C) is the main body of the SL; and yellow (zone D) is the back of the SL that is visible in some geometrical configurations due to light bending around the NS. For clarity, the accretion disk is omitted from the sketch.

Tilt effects on the polarization signatures

In this section, we study the effect of the azimuthal angle Φ\Phi and the obliquity η\eta on the energy dependence of luminosity, PD, and PA. We chose a rather wide SL with θmin⁡=60∘\theta_{\min}=60^\circ and θmax⁡=120∘\theta_{\max}=120^\circ, so that varying η\eta up to 30∘30^\circ would not break the continuity of the accretion flow. We fixed the inclination at i=75∘i=75^\circ and the SL equatorial velocity to βeq=0.35\beta_{\mathrm{eq}}=0.35; for these parameters, a relatively high PD is expected (B25). The combination of parameters used for each case is listed in Table 1.

In Figure 3, we consider three different values of the azimuthal angle, Φ\Phi, of 0∘0^\circ, 45∘45^\circ, and 90∘90^\circ. For each case, we show the dimensionless luminosity, PD, and PA for four different values of the misalignment angle η\eta. In panels (a)–(a″), the observer is in the plane formed by the NS and disk axes (we denote this plane by τ\tau). The dimensionless luminosity decreases with the obliquity

Dimensionless luminosity, PD, and PA as functions of dimensionless photon energy

Figure 3. Dimensionless luminosity xlxx l_x, PD, and PA as functions of the dimensionless photon energy, xx. Fiducial parameter values are listed in Table 1. Blue, orange, green, and red lines correspond to obliquity angles η\eta of 1∘1^\circ, 10∘10^\circ, 20∘20^\circ, and 30∘30^\circ, respectively. Azimuthal angle Φ\Phi is 0∘0^\circ in panels (a)–(a″), 45∘45^\circ in panels (b)–(b″), and 90∘90^\circ in panels (c)–(c″).

angle η\eta, while PD increases with η\eta. In all cases, the emission is polarized perpendicular to the disk.

The increase in PD is caused by the partial coverage of Zone C by the accretion disk. As η\eta increases, the contribution of Zone C to the total flux decreases, while the contributions of Zones A and B become more important. The reduced contribution of Zone C therefore leads to an increase in the net polarization. At higher energies, the contribution of Zone A becomes dominant. This explains both the increase in PD at higher energies and the slight change in PA with energy.

In panels (c)–(c″) of Figure 3, the plane τ\tau is orthogonal to the xzxz-plane, in which the observer vector k^\hat{k} lies. In this geometry, changes in obliquity have a weaker effect on PD. The main effect of changing the obliquity appears at lower energies, where PD decreases with increasing obliquity. The PA, on the other hand, changes significantly with η\eta, with PA ≃−η\simeq-\eta.

In this geometry, the accretion disk partially covers Zone B. The contribution of Zone B is most prominent at lower energies, where PD decreases with increasing obliquity. As η\eta increases, a larger fraction of Zone B is covered, reducing the contribution of Zone B to the total emission. Since the emission from Zone B is more strongly polarized than that from Zone C, this leads to a decrease in PD. The emission then comes mainly from Zones A and C, and PA is determined by the orientation of Zone A with respect to the accretion disk plane. Since this orientation depends on η\eta, this produces a correlation between the predicted PA and obliquity η\eta.

The case of Φ=45∘\Phi= 45^\circ in panels (b)–(b″) is less straightforward. It shows intermediate PD and a complex PA dependence on η\eta, as expected for a combination of the behaviors seen in panels (a)–(a″) and (c)–(c″). In this geometry, parts of both Zones B and C are covered by the accretion disk, so the mechanisms present in the two previous cases are present simultaneously. For PD, these two effects together result in little dependence of PD on η\eta. For PA, the orientation of Zone A with respect to the accretion disk plane remains a dominant factor, as in panel (c″), although the PA-η\eta relation is mildly affected by the different azimuthal angle Φ\Phi.

Parameter space study

Next, we considered the effects of changing the orbital inclination ii, the co-latitude of the SL edge θmin⁡\theta_{\min}, and the azimuthal angle Φ\Phi for a fixed obliquity η=15∘\eta= 15^\circ. The full set of parameters for each panel is given in Table 1. The results are shown in Figure 4.

Dimensionless luminosity, PD, and PA as functions of dimensionless photon energy

Figure 4. Dimensionless luminosity xlxx l_x, PD, and PA as functions of the dimensionless photon energy, xx. Fiducial parameter values are listed in Table 1. Panels (a)–(a″): the orbital inclination is varied; blue, orange, and green lines correspond to 30∘30^\circ, 60∘60^\circ, and 90∘90^\circ, respectively. Panels (b)–(b″): the co-latitude of the SL edge θmin⁡\theta_{\min} is varied; blue, orange, green, and red lines correspond to 15∘15^\circ, 30∘30^\circ, 60∘60^\circ, and 75∘75^\circ, respectively. Solid lines correspond to η=15∘\eta= 15^\circ, while dashed lines correspond to the aligned case with η=0\eta= 0 from B25. Panels (c)–(c″): the azimuthal angle Φ\Phi is varied; the lines, colored according to the inferno palette, correspond to −135∘-135^\circ, −90∘-90^\circ, −45∘-45^\circ, 0∘0^\circ, 45∘45^\circ, 90∘90^\circ, 135∘135^\circ, and 180∘180^\circ, respectively.

Panels (a)–(a″) illustrate the effect of changing the orbital inclination iorbi_{\rm orb}. The results show the standard trend of PD increasing with orbital inclination and PA varying slightly around the direction orthogonal to the disk plane (B25). In the case of i=30∘i = 30^\circ, all four Zones contribute to the flux, while for the other two cases, Zone D does not. Panel (a) shows a shift in the peak energy, which is associated with the Doppler effect. For a fixed velocity βeq\beta_{\rm eq}, the Doppler effect is stronger at higher inclinations, because the projection of the velocity onto the direction to the observer is larger at higher inclinations in the current configuration of the system.

In panels (b)–(b″), we showed the impact of the SL width by varying the edge co-latitude θmin⁡\theta_{\min}. For comparison, we also showed the corresponding results for aligned star with dashed lines (B25). Since dimensionless luminosity is normalized to the surface area of the SL, panel (b) shows almost no effect of θmin⁡\theta_{\min} on xlxx_{\rm lx}. Panel (b’) shows that, similarly to the aligned case (B25), the narrower the SL, the higher the PD. In the case of θmin⁡=15∘\theta_{\min} = 15^\circ, most of the NS surface is covered by the SL, and the geometry of the SL approaches a sphere, which contributes to depolarization (B25). This effect weakens with increasing θmin⁡\theta_{\min}.

The misalignment in this case contributes to a minor increase in PD for θmin⁡=75∘\theta_{\min} = 75^\circ and θmin⁡=60∘\theta_{\min} = 60^\circ, while the emission from a wider SL seems almost unaffected by the misalignment. Similarly, PA is mildly affected by the misalignment, with the difference being more noticeable for narrower SLs with θmin⁡=75∘\theta_{\min} = 75^\circ and θmin⁡=60∘\theta_{\min} = 60^\circ. The reason behind this change with respect to the case of η=0∘\eta= 0^\circ again lies in the partial covering of Zone C by the accretion disk and the slight asymmetry introduced by observing the system from Φ=45∘\Phi= 45^\circ. This effect is less present for a wider SL, where emission is depolarized.

In panels (c)–(c”), we show the effect of varying the azimuthal angle Φ\Phi. The dimensionless luminosity shown in panel (c) strongly depends on Φ\Phi. For Φ=0∘\Phi= 0^\circ or 180∘180^\circ, the problem is axially symmetric, similar to the case presented in Figure 3, panels (a)–(a’’). Zones A and B contribute equally to the flux. However, for 0∘<Φ<180∘0^\circ< \Phi< 180^\circ, Zone B is partially or completely covered by the accretion disk, and hence the peak energy increases. For −180∘<Φ<0∘-180^\circ< \Phi< 0^\circ, the situation is reversed: Zone A is partially or completely covered by the accretion disk, and the peak energy decreases. Since the luminosity is normalized to the full surface area of the SL, not to the visible part, the peak luminosity also changes significantly, increasing by an order of magnitude between the case of Φ=0∘\Phi= 0^\circ, where Zone C is covered by the accretion disk, and the case of Φ=180∘\Phi= 180^\circ, where a larger fraction of Zone C is visible, since the star is tilted in the direction opposite to the observer.

We note that for Φ=0∘\Phi= 0^\circ and Φ=−45∘\Phi= -45^\circ, the PD is higher than in other cases. The PA varies within a range of approximately 20∘20^\circ as Φ\Phi changes, first slowly decreasing as Φ\Phi increases from −45∘-45^\circ to 135∘135^\circ, and then slowly increasing for the other hemisphere. This is caused by the fact that PA mostly depends on the minimal co-latitude that is covered by the SL, which changes slowly with the azimuthal angle in the misaligned case. For a larger obliquity angle η\eta, a larger variation in PA is expected.

Monochromatic polarization as a function of orientation

After studying the energy dependence of spectropolarimetric properties, we fixed the photon energy and calculated PD and PA for all possible combinations of obliquity η\eta and azimuthal angle Φ\Phi. We linked the co-latitude of the SL edge to the obliquity angle through the relation θmin⁡=90∘−η\theta_{\min} = 90^\circ- \eta, so that there is never a gap between the SL and the accretion disk. In this configuration, the SL is wider for systems with larger misalignment. We kept the same equatorial flow velocity βeq=0.35\beta_{\rm eq} = 0.35. To characterize the average PD and PA in the IXPE energy range, we chose to study monochromatic polarization at E=5E = 5 keV. In the previous section, we used the dimensionless energy xx, and since the energy is now expressed in keV, we also had to fix the effective temperature TeffT_{\rm eff} and the color correction fcf_{\rm c} for the SL. Based on spectroscopic studies of WMNSs, we adopted fc Teff=2f_{\rm c}\,T_{\rm eff} = 2 keV. As before, all the parameter values for each simulation are listed in Table 1.

In Figure 5, the results are shown for three different orbital inclinations, ii, of 30∘30^\circ, 50∘50^\circ, and 70∘70^\circ. The case of the lowest orbital inclination presented in panel (a) shows PD <0.5%< 0.5\%, except for the region of η<15∘\eta< 15^\circ. For small η\eta, the width of the SL plays a crucial role, significantly increasing the polarization. Panels (b) and (c) show that, for moderate or high inclination, PD can remain higher than 1% even at larger values of η\eta, which in this simulation correspond to a rather wide SL. We note that PD reaches its maximum for −45∘<Φ<0-45^\circ< \Phi< 0. Contrary to the results shown in panels (a’), (b’), and (c’) of Figure 3, PD is higher for smaller obliquity angles in this simulation. Here, η\eta is connected to the SL width, and the effect of the SL width on PD dominates the behavior, while in Figure 3, the SL width was fixed. The PA is strongly influenced by the obliquity, as seen in panels (b”) and (c”) of Figure 3. The behavior of the polarimetric properties shows a common topology for different inclinations; for instance, the PD maxima occur in similar regions in panels (b) and (c). PA depends strongly on both Φ\Phi and η\eta at all considered inclinations.

Contour plots of PD and PA as functions of obliquity and azimuthal angle

Figure 5. Contour plots of PD and PA as functions of obliquity η\eta and azimuthal angle Φ\Phi. Panels (a)–(a’): orbital inclination i=30∘i = 30^\circ; panels (b)–(b’): i=50∘i = 50^\circ; panels (c)–(c’): i=70∘i = 70^\circ. Remaining parameter values are listed in Table 1.

Next, we investigated the probability of detecting the PD higher than the threshold for a fixed obliquity η\eta. For this study, we assumed a flat distribution for both cos⁡i\cos i and Φ\Phi. The results are shown in Figure 6. We show the constant PD contours for two values of obliquity, η\eta, of 15∘15^\circ and 30∘30^\circ. Contrary to panels (a’) and (b’) of Figure 3, where the highest PD was expected for η=30∘\eta= 30^\circ, here we observe the decrease of PD with misalignment; this is due to the fact that SL is wider for η=30∘\eta= 30^\circ, since we set θmin⁡=90∘−η\theta_{\min} = 90^\circ- \eta. The calculated probabilities of observing a PD higher than the threshold value are given in Table 2. We considered six obliquity values and four PD levels. We did not consider η>30∘\eta> 30^\circ, since PD drops rapidly at higher obliquity due to an increase in the SL width. Since the probability distribution of η\eta is likely not flat, to understand the true probability of observing the system at a given level of PD, we need to convolve the reported probabilities with the probability distribution of η\eta in the WMNS population. We can, however, conclude that only for a few values of η\eta does the probability of observing a PD higher than 1% exceed 20%, and the 2% PD level is rarely reached, with a probability exceeding 1% only for η=5∘\eta= 5^\circ.

Contour plots of PD and PA as functions of the azimuthal angle $\Phi$ and the cosine of the orbital inclination $\cos i$

Figure 6. Contour plots of PD and PA as functions of the azimuthal angle Φ\Phi and the cosine of the orbital inclination cos⁡i\cos i. Panels (a)–(a’): obliquity η=15∘\eta= 15^\circ; panels (b)–(b’): η=30∘\eta= 30^\circ. Remaining parameter values are listed in Table 1.

PD (%)η\eta (deg)51015202530
≥0.5\ge0.5395048554636
≥1.0\ge1.028252117127.8
≥1.5\ge1.515129.26.13.00.4
≥2.0\ge2.02.90.80.00.00.00.0

Table 2. Probability (in %) of detecting PD higher than the threshold for different obliquity values.

Discussion

The results presented in Sect. 3 show several important trends. Regarding the spectrum, the main result is that misalignment affects the spectral shape, an effect that should be taken into account when performing the spectral decomposition. For the PD, we note that breaking the axial symmetry increases the expected PD with respect to the aligned case presented in B25, with PD exceeding 2% for some parameter combinations (see Table 2 for examples). Regarding the PA, we conclude that misalignment in the system allows the polarization plane to take any orientation.

Before comparing the model predictions with the observational results, it is important to discuss the possibility of misalignment in a WMNS system. When an X-ray binary is formed following the collapse of a normal star into a compact object, the rotation axis of the compact object is not required to be aligned with the orbital axis [48]. The accretion process reduces the obliquity, since angular momentum is transferred from the disk to the NS via the accretion flow. The timescale for the alignment process depends on the mass accretion rate, magnetic field strength, rotation rate of the NS, and other parameters.

Theoretical expectations for the alignment time in binaries are discussed in the literature for several subclasses of sources: for instance, Kool & van Paradijs [9] estimated the alignment time for millisecond pulsars at ≈106\approx10^6 years, while Abolmasov et al. [1] suggests a significantly shorter alignment time for strongly magnetized NSs. Martin et al. [28] estimated an alignment time of 10710^7 years for the black hole X-ray binary GRO J1655–40 is reported. However, no theoretical expectations have been derived for WMNSs. Although most of these objects are considered to be rather old (e.g. the age estimate of Cyg X-2 is 4×1084 \times10^8 yr; King & Ritter [23]), some are known to be considerably younger, and possibly young enough to remain misaligned. For instance, the age of Sco X-1 is estimated to be 7×1067 \times10^6 yr (Kar et al. [22]), while Cir X-1 is less than 5×1035 \times10^3 yr old (Heinz et al. [17]). The alignment time can also be extended by additional factors related to binary evolution and by events occurring during it. For instance, if the accretion process has been episodic, or if the binary system is particularly wide, the accretion-driven alignment could take a significantly longer time (Laycock et al. [25]).

Cir X-1 is the first and most compelling candidate for a potentially misaligned WMNS. Apart from being the youngest known WMNS system, Cir X-1 is known to have precessing jets (Cowley et al. 2025) and a high eccentricity of 0.40.4–0.450.45 (Jonker et al. [21]; Johnston et al. [20]), with even higher values reported in earlier works, e.g., 0.940.94 in Tauris et al. [45]. The presence of a kick during the supernova event in this system has been discussed as a possible explanation for both the jets and the eccentricity, and with an age of less than 10410^4 yr, there may not have been sufficient time for the NS rotational axis to align with the orbital axis through accretion.

The IXPE observation of Cir X-1 in August 2023 revealed strong PA variability with spectral hardness and source state, as well as a PA that was misaligned with both the assumed disk plane and the jet axis. Obliquity in the system has been suggested as one of the possible explanations for the observed polarimetric behavior. Rankin et al. [36] suggest that, based on the temporal evolution of PA, Cir X-1 exhibited different accretion-flow geometries during the observations, with the geometry during the part of observation labeled P3 including an SL. During that part of the observation, Cir X-1 had a PD of 1.4% and a PA =−12∘= -12^\circ neither orthogonal nor aligned with the jet position angle reported to be between −40∘-40^\circ and −70∘-70^\circ. If we assume the jet direction to be orthogonal to the accretion disk plane, the observed PA would correspond to 30∘30^\circ and 60∘60^\circ in our simulations. As shown in Figure 5, such a PA is expected for an azimuthal angle Φ\Phi between ≈−135∘\approx-135^\circ and ≈−45∘\approx-45^\circ and an obliquity η\eta larger than ≈30∘\approx30^\circ. More precise constraints on η\eta are difficult to derive due to the uncertainty in the PA. We note that the exact numbers also depend on the inclination of the system and other parameters that are assumed rather than inferred, in the simulations. Accounting for both PD and PA does not tighten the constraints; Figure 5 illustrates that PD does not reach 1.4% within the stated ranges of obliquity and azimuthal angles in our simulation, at least for the selected set of parameters. We can, however, conclude from Figure 5 that higher inclinations are favored, since PD in the selected region rises with inclination. This could be interpreted as a hint of a relatively high inclination of the system. However, we note that the PD prediction is strongly affected by assumptions regarding the SL structure and composition; while we consider only scattering off electrons, introducing ions and accounting for absorption in the SL could significantly increase the expected PD [37]. Given these uncertainties, we do not derive any tighter constraints on the Cir X-1 geometry from the PD predictions.

Apart from Cir X-1, a few other systems have exhibited signs of misalignment based on IXPE observations. For instance, in GX 5−1, a swing by ≈ 50∘50^\circ between the PA of the disk and the Comptonized components was reported Fabiani et al. [12]. If we assume the disk to be polarized in the plane of the disk Loktev et al. [26], corresponding to a 90∘90^\circ PA in this paper, then the Comptonized component is polarized in the direction of ≈ 40∘40^\circ, which can be reproduced by our model. Although both of these systems are considered old, with an approximate age of 10810^8 yr, little is known about the duration of their active accretion phase. We neither favor nor rule out misalignment as a possibility in these systems; rather, we provide a model to investigate the polarimetric properties of these objects under the assumption of misalignment. We look forward to studying the results of further spectropolarimetric observations of these systems.

Summary

We developed a model for the spectropolarimetric properties of the emission of a SL on a tilted WMNS, whose rotational axis is not aligned with that of the binary system. We investigated how luminosity, PD, and PA depend on energy and on the geometrical parameters of the system, such as the obliquity angle η\eta, the azimuthal angle Φ\Phi, the inclination of the binary system ii, and the co-latitude of the SL edge θmin⁡\theta_{\min}.

We conclude that the expected polarimetric properties of the SL emission depend strongly on the geometrical parameters of the system. First, we find that breaking the axial symmetry contributes to an increase in the PD of the SL emission. Additionally, we show that misalignment in the system could explain why the observed PA is neither aligned with nor orthogonal to the assumed disk plane or binary rotational axis. Consistent with the aligned case studied in B25, PD increases with energy and inclination and decreases with increasing SL width. We find that a higher PD is predicted for azimuthal angles in the range Φ=−45∘\Phi= -45^\circ–0∘0^\circ. The effect of the obliquity angle strongly depends on the SL width, which is connected to the mass accretion rate Inogamov & Sunyaev [19]. For luminous systems with a wider SL, PD is higher for larger values of η\eta, as seen in Figure 3; in less luminous systems, where the width of the layer is connected to the obliquity as shown in Sect. 3.3, PD is higher for lower obliquity.

In recent years, observations of several systems have shown indications of misalignment, and in this paper we predict their polarimetric properties under the assumption of misalignment. The formalism derived here can be used to interpret existing and upcoming spectropolarimetric observations of WMNSs. The misalignment scenario can be realized in cases in which transfer of angular momentum from the accretion disk has not significantly altered the orientation of the NS rotational axis. The most natural candidates for this scenario are young systems such as Cir X-1. Older systems like GX 13+1 and other WMNSs require episodic mass transfer or additional mechanisms to reduce the effect of the accretion process on the NS spin; in such cases, a non-negligible obliquity may persist even in older systems.

Acknowledgements. This research was supported by the grant 00240328 of the Finnish Cultural Foundation (AB), by the Research Council of Finland Centre of Excellence in Neutron-Star Physics (grant 374064) and grants 355672 and 372881 (AV).

Polarized emission from an aligned spreading layer

To calculate the polarized emission from the SL, we first derived an equation for the polarized flux coming from a small surface element dFEdF_{\mathrm{E}}, and then integrated that emission over the whole visible surface of the SL in the coordinate system associated with the NS rotation axis. Main equations have been derived in Poutanen [32] and Suleimanov et al. [43]. For the assumed spherical NS, the surface normal n^\hat{\mathbf{n}} coincides with the radius-vector of the element r^\hat{\mathbf{r}} and thus the angle ψ\psi between n^\hat{\mathbf{n}} and the direction to the observer k^\hat{\mathbf{k}} is

cos⁡ψ≡k^⋅n^=cos⁡i∗cos⁡θ+sin⁡i∗sin⁡θcos⁡ϕ,(23)\cos\psi\equiv\hat{\mathbf{k}}\cdot\hat{\mathbf{n}}=\cos i_{*}\cos\theta+\sin i_{*}\sin\theta\cos\phi, \tag*{(23)}

where ϕ=0\phi=0 when the element was closest to the observer. The emission angle α(ψ)\alpha(\psi) (i.e., the angle to the surface normal in the external frame) was calculated using Beloborodov [2] approximation

cos⁡α(ψ)≡k^0⋅n^≈1−(1−u)(1−cos⁡ψ),(24)\cos\alpha(\psi)\equiv\hat{\mathbf{k}}_{0}\cdot\hat{\mathbf{n}}\approx1-(1-u)(1-\cos\psi), \tag*{(24)}

with the visibility condition for the surface element being cos⁡α>0\cos\alpha>0. Here, u=RS/Ru=R_{\mathrm{S}}/R is the NS compactness, and k^0\hat{\mathbf{k}}_{0} is the unit vector of the photon momentum close to the surface,

k^0=sin⁡α k^+sin⁡(ψ−α) n^sin⁡ψ.(25)\hat{\mathbf{k}}_{0}=\frac{\sin\alpha\,\hat{\mathbf{k}}+\sin(\psi-\alpha)\,\hat{\mathbf{n}}}{\sin\psi}. \tag*{(25)}

Similarly to B25, we defined the velocity of the material in the SL by the direction of the unit vector v^=(−sin⁡ϕ,cos⁡ϕ,0)∗\hat{\mathbf{v}}=(-\sin\phi,\cos\phi,0)_{*} and the amplitude (in units of speed of light) as a function of latitude

β(θ)=βeqsin⁡θ=A vkeplcsin⁡θ=Au2(1−u)sin⁡θ,(26)\beta(\theta)=\beta_{\mathrm{eq}}\sin\theta=\frac{A\,v_{\mathrm{kepl}}}{c}\sin\theta=A\sqrt{\frac{u}{2(1-u)}}\sin\theta, \tag*{(26)}

with A<1A<1 being a proportionality coefficient that scales equatorial velocity relative to the Keplerian velocity vkeplv_{\mathrm{kepl}} in the Schwarzschild metric (Luminet [27]). The angle between the velocity vector and the photon direction is then (Poutanen & Gierliński [33]):

cos⁡ξ=v^⋅k^=sin⁡αsin⁡ψv^⋅k^=−sin⁡αsin⁡ψsin⁡i∗sin⁡ϕ.(27)\cos\xi=\hat{\mathbf{v}}\cdot\hat{\mathbf{k}}=\frac{\sin\alpha}{\sin\psi}\hat{\mathbf{v}}\cdot\hat{\mathbf{k}}=-\frac{\sin\alpha}{\sin\psi}\sin i_{*}\sin\phi. \tag*{(27)}

We calculated the observed flux at energy EE from the surface element with area dS=R2dcos⁡θdϕdS=R^{2}d\cos\theta d\phi as follows:

dFE=IEdΩobs=Dcos⁡αdSD2,(28)dF_{\mathrm{E}}=I_{\mathrm{E}}d\Omega_{\mathrm{obs}}=\mathcal{D}\cos\alpha\frac{dS}{D^{2}}, \tag*{(28)}

where D\mathcal{D} is the lensing factor that is equal to one in the Beloborodov approximation.

To account accurately for the relativistic effects of the matter rotation, we moved to the frame co-rotating with the SL matter. We considered the SL element to be an electron-dominated semi-infinite slab (Chandrasekhar [4]; Sobolev [42]) so that we could compute the angular distribution and polarization of the escaping radiation. We assumed the local intensity IE′(α′,θ)I'_{\mathrm{E}}(\alpha',\theta) to have a diluted blackbody shape, same as in Suleimanov et al. [43] and B25, given by Eq. (7). The angle α′\alpha' made by the photon momentum with the surface normal in the co-rotating frame is related to the emission angle α\alpha defined in Eq. (A.2) as (Poutanen & Gierliński [33])

cos⁡α′=δcos⁡α,(29)\cos\alpha'=\delta\cos\alpha, \tag*{(29)}

where δ\delta is the Doppler factor

δ=1γ(1−βcos⁡ξ)(30)\delta=\frac{1}{\gamma(1-\beta\cos\xi)} \tag*{(30)}

and γ\gamma is the Lorentz factor

γ(θ)=11−β2(θ).(31)\gamma(\theta)=\frac{1}{\sqrt{1-\beta^{2}(\theta)}}. \tag*{(31)}

The local intensity IE′I'_{\mathrm{E}} can depend on co-latitude θ\theta but we consider here the effective temperature and the color correction factors to be constant throughout the SL. The observed intensity is related to the local one:

IE=(EE′)3IE′(α′,θ)=(δ1−u)3IE′.(32)I_{\mathrm{E}}=\left(\frac{E}{E'}\right)^{3}I'_{\mathrm{E}}(\alpha',\theta)=\left(\delta\sqrt{1-u}\right)^{3}I'_{\mathrm{E}}. \tag*{(32)}

The total observed flux coming from the surface element was calculated as

dFE=R2D2cos⁡α D(δ1−u)3IE′(α′,θ)dcos⁡θ dϕ,(33)dF_{\mathrm{E}}=\frac{R^{2}}{D^{2}}\cos\alpha\,\mathcal{D}\left(\delta\sqrt{1-u}\right)^{3}I'_{\mathrm{E}}(\alpha',\theta)d\cos\theta\,d\phi, \tag*{(33)}

where DD is the distance to the source.

Polarimetric properties of the SL emission can be described by the Stokes vector:

dF(E)=(dFI(E)dFQ(E)dFU(E))=dFE(1Pcos⁡2χPsin⁡2χ),(34)d\mathbf{F}(E)= \begin{pmatrix} dF_{\mathrm{I}}(E)\\ dF_{\mathrm{Q}}(E)\\ dF_{\mathrm{U}}(E) \end{pmatrix} =dF_{\mathrm{E}} \begin{pmatrix} 1\\ P\cos2\chi\\ P\sin2\chi \end{pmatrix}, \tag*{(34)}

where PP is the PD of the escaping radiation, and χ\chi is the PA. We calculated PD using the approximation from Viironen & Poutanen (2004) for a semi-infinite electron-scattering-dominated atmosphere (Chandrasekhar [4]):

P=Pes(α′)=−1−cos⁡α′1+3.582cos⁡α′ 0.1171,(35)P=P_{\mathrm{es}}(\alpha')=-\frac{1-\cos\alpha'}{1+3.582\cos\alpha'}\,0.1171, \tag*{(35)}

and the PA with the formulae derived by Poutanen [32]:

tan⁡χ=sin⁡θsin⁡ϕ+βA−sin⁡i∗cos⁡θ+cos⁡i∗sin⁡θcos⁡ϕ−βsin⁡ϕ C,(36)\tan\chi=\frac{\sin\theta\sin\phi+\beta A}{-\sin i_{*}\cos\theta+\cos i_{*}\sin\theta\cos\phi-\beta\sin\phi\,C}, \tag*{(36)}

where

A=sin⁡ψsin⁡αB+cos⁡α−cos⁡ψsin⁡αsin⁡ψ(cos⁡ϕ−Bcos⁡ψ),B=sin⁡i∗sin⁡θ+cos⁡i∗cos⁡θcos⁡ϕ,C=sin⁡ψsin⁡αcos⁡θ+cos⁡α−cos⁡ψsin⁡αsin⁡ψ(cos⁡i∗−cos⁡θcos⁡ψ).(37)\begin{aligned} A&=\frac{\sin\psi}{\sin\alpha}B+\frac{\cos\alpha-\cos\psi}{\sin\alpha\sin\psi}(\cos\phi-B\cos\psi),\\ B&=\sin i_{*}\sin\theta+\cos i_{*}\cos\theta\cos\phi,\\ C&=\frac{\sin\psi}{\sin\alpha}\cos\theta+\frac{\cos\alpha-\cos\psi}{\sin\alpha\sin\psi}(\cos i_{*}-\cos\theta\cos\psi). \tag*{(37)} \end{aligned}

These equations account for the effects of rotation of polarization plane because of relativistic motion as well as for light bending in the Schwarzschild metric.

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