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Frame-dragging

Frame-dragging, also known as the Lense–Thirring effect, is a phenomenon predicted by Einstein's theory of general relativity in which a rotating massive object, such as a planet or star, warps and twists the surrounding spacetime, thereby dragging nearby inertial frames and objects along in the direction of its rotation.^[1] This gravitomagnetic effect arises from the interaction between the object's angular momentum and the curvature of spacetime, analogous to how a magnetic field arises from electric currents, and it manifests as a precession or shift in the orientation of gyroscopes, orbits, or test particles near the rotating body.^[2] The magnitude of frame-dragging diminishes rapidly with distance from the source, making it most pronounced in strong gravitational fields close to compact objects like black holes or rapidly spinning neutron stars.^[1] The effect was first theoretically derived in 1918 by Austrian physicists Josef Lense and Hans Thirring, who solved Einstein's field equations for a slowly rotating spherical mass to describe how its rotation influences the motion of nearby bodies, such as planets or moons.^[3] Their work, building directly on Einstein's 1916 formulation of general relativity, predicted that the orbital plane of a satellite around Earth would experience a nodal precession of approximately 31 milliarcseconds per year due to frame-dragging, in addition to classical effects like oblateness-induced precession.^[1] This prediction embodies Mach's principle, suggesting that the local inertial frame is influenced by the distant distribution of matter and rotation in the universe, though frame-dragging specifically captures the local rotational influence of the central body.^[2] Experimental confirmation of frame-dragging has been achieved through several high-precision measurements, validating general relativity to within a few percent. NASA's Gravity Probe B mission, launched in 2004, used four superconducting gyroscopes in polar orbit to detect the effect around Earth, reporting a frame-dragging drift rate of −37.2 ± 7.2 milliarcseconds per year in 2011, consistent with the predicted −39.2 milliarcseconds per year.^[4] Earlier ground-based and satellite laser ranging tests, including those with the LAGEOS satellites from 1993 to 2003, measured the effect with about 10% uncertainty, aligning with predictions to 99% accuracy when combined with gravitational models from the GRACE mission.^[2] More recently, in 2020, observations of the binary pulsar PSR J1141−6545 revealed frame-dragging induced by a fast-rotating white dwarf companion, with the orbital inclination evolving as expected from the Lense–Thirring precession, providing constraints on the system's formation and further corroborating the theory in a stellar context.^[5] These tests not only confirm the existence of frame-dragging but also highlight its role in phenomena like the alignment of accretion disks around black holes and the behavior of jets in quasars.^[1]

Background and History

Theoretical Prediction

The theoretical prediction of frame-dragging arose shortly after the completion of Albert Einstein's general theory of relativity in 1915, as researchers began exploring solutions to the Einstein field equations for rotating masses. In these early investigations, the rotation of a massive body was found to generate a dynamic distortion of spacetime, distinct from the static curvature produced by non-rotating masses. This effect, later termed frame-dragging, implies that the inertial frames of reference in the vicinity of the rotating body are pulled along with its motion, akin to the twisting of spacetime fabric.^[6] Hans Thirring provided the first explicit calculation of this phenomenon in his 1918 paper, where he examined the influence of a rotating spherical shell of mass on test particles inside it. Thirring demonstrated that the shell's rotation induces a "twisting" of spacetime, leading to apparent forces on the test particles that mimic the dragging of their local inertial frames. This prediction highlighted how the angular momentum of the rotating mass alters the geometry of spacetime in a way that affects the motion of objects within, setting frame-dragging apart from purely gravitational attraction.^[7] Building on Thirring's work, Josef Lense and Hans Thirring collaborated on a follow-up paper later in 1918, formalizing the effect specifically for scenarios involving slow rotation and weak gravitational fields. Their analysis extended the interior solution to the exterior region around a rotating central body, predicting that the dragging would cause a precession in the orbits of surrounding particles, such as planets or moons. This collaborative effort established frame-dragging as a key testable prediction of general relativity, emphasizing its role in coupling the rotation of the source mass to the orientation of distant inertial frames.^[8]

Historical Development

The concept of frame-dragging emerged from Albert Einstein's early explorations of general relativity, particularly his work on rotating coordinate systems. In 1913, collaborating with Michele Besso, Einstein derived a Coriolis-like force inside a rotating spherical shell of mass within the framework of the Entwurf theory, an intermediate version of general relativity, calculating a dragging coefficient that was half the value later obtained in the complete theory.^[6] This work highlighted how rotation could influence local inertial frames, influencing the recognition of frame-dragging effects in the full general theory of relativity developed by 1916.^[6] The formal prediction of frame-dragging in general relativity came in 1918 through the contributions of Josef Lense and Hans Thirring. Guided by Einstein's correspondence, Thirring calculated the gravitomagnetic field produced by a rotating mass, focusing on far-field effects and the precession induced in test particles or gyroscopes.^[6] Lense extended these results to astronomical applications, such as orbital perturbations around the Sun, and the effect became known as the Lense-Thirring effect.^[6] Their analysis, published in the Physicalische Zeitschrift, established the theoretical foundation for frame-dragging but relied on linear approximations, neglecting higher-order terms in the metric.^[6] A 2007 historical analysis by Herbert Pfister has proposed renaming the effect the Einstein–Thirring–Lense effect to better reflect Einstein's pivotal role, including his 1913 collaboration with Besso and guidance to Thirring, though Lense–Thirring remains the conventional name.^[6] Mid-20th-century developments revived interest in testing frame-dragging experimentally. In 1959, Leonard Schiff at Stanford University proposed using ultra-precise gyroscopes in space to measure the effect caused by Earth's rotation, conceiving the foundational idea for what would become the Gravity Probe B mission.^[9] Post-1960 advancements extended frame-dragging to more complex scenarios, notably in strong gravitational fields. Roy Kerr's 1963 solution for the metric describing spacetime around a rotating black hole incorporated frame-dragging intrinsically, revealing phenomena like the ergosphere where spacetime is forced to rotate with the black hole.^[10] Numerical simulations in the strong-field regime, beginning in the late 20th century, further refined these predictions by modeling nonlinear interactions in rotating systems.^[11] Early theories identified gaps, such as the omission of higher-order gravitational terms beyond the linear approximation, which affected accuracy in dense or rapidly rotating configurations. These limitations were later addressed through advancements in gravitomagnetism, expanding the analogy between gravity and electromagnetism to include post-linear corrections and better integrate frame-dragging into broader general relativistic calculations, as formalized in works like the 1973 textbook by Misner, Thorne, and Wheeler.^[12]

Physical Interpretation

Gravitomagnetic Analogy

In general relativity, the gravitomagnetic analogy offers an intuitive framework for understanding frame-dragging by paralleling gravitational effects with those in electromagnetism. A rotating mass generates a gravitomagnetic field, much like a rotating charged body produces a magnetic field from the motion of electric charges. This analogy, first proposed by Oliver Heaviside in the late 19th century and later adapted to general relativity, highlights how mass currents—arising from rotation—create these fields in spacetime.^[13] Frame-dragging emerges as the spacetime equivalent of a current induced by this gravitomagnetic field, influencing the orientation of nearby objects.^[14] Within this framework, linear momentum in general relativity corresponds to gravitoelectric fields, analogous to electric fields generated by stationary charges, while angular momentum produces gravitomagnetic fields, akin to magnetic fields from moving charges. This correspondence leads to force-like effects on test masses that resemble the Lorentz force in electromagnetism, where the motion of a particle through the gravitomagnetic field induces a deflection.^[13] Qualitatively, a spinning mass twists nearby inertial frames in a manner similar to how magnetic field lines align compass needles, providing a visualizable picture of the dragging effect without requiring full geometric interpretations.^[14] Despite its utility, the gravitomagnetic analogy has inherent limitations. General relativity's effects are inherently nonlinear, meaning strong fields do not simply superpose as they do in the linear Maxwell equations of electromagnetism, and gravitational interactions are universal, affecting all masses indiscriminately rather than selectively like charged particles in electromagnetic fields. These differences underscore that the analogy serves primarily as a pedagogical tool in the weak-field regime, rather than a complete equivalence.^[13]

Spacetime Dragging Mechanism

In general relativity, frame-dragging arises as a geometric consequence of a rotating mass-energy distribution warping the structure of spacetime, such that nearby geodesics— the straightest possible paths for freely falling objects—are pulled along in the direction of the rotation axis. This twisting of spacetime metric components encodes a rotational influence that alters the local geometry, compelling inertial observers and test particles to experience a cumulative azimuthal shift in their paths relative to non-rotating coordinates.^[15] Unlike geodetic precession, which stems from the parallel transport of vectors along curved geodesics due to the orbital motion in a static gravitational field, frame-dragging specifically isolates the rotational component induced by the source's spin, manifesting as an additional torsion in spacetime that does not occur for non-rotating masses.^[16]^[15] A illustrative thought experiment involves a test particle placed at rest relative to asymptotically distant stars near a rotating mass; over time, the particle's local coordinate system—defined by its inertial frame—rotates with respect to those fixed distant stars due to the local spacetime torsion, even though the particle itself follows a geodesic.^[15]^[17] This dragging is sourced fundamentally by the angular momentum tensor within the stress-energy distribution, which contributes off-diagonal terms to the spacetime metric proportional to the rotation; without angular momentum, as in spherically symmetric non-rotating configurations like the Schwarzschild metric, no such frame-dragging effect occurs.^[17]

Mathematical Formulation

Weak-Field Derivation

In the weak-field limit of general relativity, frame-dragging arises from the linearised Einstein field equations under the harmonic gauge condition, where the metric perturbation satisfies \partial^\mu \bar{h}_{\mu\nu} = 0 with \bar{h}_{\mu\nu} = h_{\mu\nu} - \frac{1}{2} \eta_{\mu\nu} h. The equations simplify to \Box \bar{h}_{\mu\nu} = -\frac{16\pi G}{c^4} T_{\mu\nu}, allowing solutions analogous to those in electromagnetism for slow-motion sources.^[18] For stationary configurations, the time-independent solution yields \bar{h}_{\mu\nu}(\vec{x}) = \frac{4G}{c^4} \int \frac{T_{\mu\nu}(\vec{x}')}{|\vec{x} - \vec{x}'|} d^3x'.^[19] The gravitomagnetic effects emerge from the spatial-temporal components, defining the gravitomagnetic potential as h_{0i} = -\frac{4G}{c^4} \int \frac{T^{0i}(\vec{x}')}{|\vec{x} - \vec{x}'|} d^3x', where T^{0i} represents the mass-energy current density.^[18] This potential \vec{A}_g (with A_{g,i} = -h_{0i} c / 4) parallels the magnetic vector potential in electromagnetism, capturing the influence of rotating mass distributions. The associated gravitomagnetic field is then \vec{B}_g = \nabla \times \vec{A}_g, which for a localized mass current density \mathbf{J} in the far field takes the form \vec{B}_g = -\frac{G}{c^3} \nabla \times \left( \frac{\mathbf{J}}{r} \right).^[19] This field induces frame-dragging through the precession of nearby test systems, with the angular velocity derived from the geodesic deviation or spin transport equations in the linearised theory. For a test gyroscope at rest relative to the distant stars, the frame-dragging precession is \vec{\Omega} = -\frac{1}{2} \vec{B}_g. The full precession for moving gyroscopes includes additional geodetic terms from the coupling of velocity and gravitoelectric field, but the gravitomagnetic contribution remains -\frac{1}{2} \vec{B}_g.^[18] Applying boundary conditions for an isolated rotating body with total angular momentum \vec{J}, the far-field metric perturbation incorporates the dipole term, yielding the Lense-Thirring form in the line element:

ds^2 = -\left(1 - \frac{2GM}{c^2 r}\right) c^2 dt^2 + \left(1 + \frac{2GM}{c^2 r}\right) (dx^2 + dy^2 + dz^2) - \frac{4 G }{c^3 r^3} \left( \vec{J} \times \vec{r} \cdot d\vec{x} \right) c dt.

This cross term directly encodes the frame-dragging, twisting the spacetime coordinates around the rotating source.^[19]

Lense-Thirring Effect in Rotating Shells

The Lense-Thirring effect in the context of a rotating spherical shell arises from solving the linearized Einstein field equations in the vacuum regions inside and outside a thin, uniformly rotating shell of mass M, radius R, and angular velocity \vec{\omega} directed along the z-axis. This idealized setup, first analyzed by Hans Thirring, models the shell as an infinitely thin surface with constant surface mass density, neglecting higher-order terms in the rotation speed and gravitational potential (weak-field, slow-rotation approximation). The metric perturbations are computed relative to Minkowski spacetime, capturing the gravitomagnetic contributions due to the shell's rotation.^[7] Inside the shell (r < R), the solution yields a uniform frame-dragging field, characterized by a constant angular velocity \vec{\Omega} that represents the vorticity of the spacetime, analogous to a uniform magnetic field within a rotating charged shell in electromagnetism. Specifically, \vec{\Omega} = \frac{4 G M \vec{\omega}}{3 c^2 R}, where G is the gravitational constant and c is the speed of light. This uniform dragging implies that inertial frames throughout the interior precess at the same rate, independent of position. The derivation involves integrating the gravitomagnetic potential over the shell's surface, resulting in a constant interior field proportional to the shell's total angular momentum J = \frac{2}{3} M R^2 \omega.^[7]^[6] Outside the shell (r > R), the frame-dragging field decays with a dipole-like profile, \vec{\Omega} = \frac{G}{c^2} \frac{3 (\vec{J} \cdot \hat{r}) \hat{r} - \vec{J}}{r^3}, mirroring the far-field magnetic dipole generated by a rotating charged sphere. This expression, refined in the joint work of Josef Lense and Thirring, shows the dragging angular velocity falling off as $1/r^3, with the leading term at the equator given by \Omega \approx \frac{2 G J}{c^2 r^3}. The exterior solution satisfies the vacuum Einstein equations and matches continuously to the interior at r = R, confirming the shell's rotation induces a long-range gravitomagnetic influence.^[20]^[6] An exact coordinate transformation further illuminates the interior solution: the metric inside the shell can be expressed in coordinates rotating rigidly with angular velocity \vec{\Omega}, reducing to the flat Minkowski metric in those coordinates. This demonstrates that the spacetime inside is locally flat but globally twisted by the shell's rotation, with observers at rest in the original coordinates experiencing a uniform Coriolis-like force proportional to \frac{8 G M \omega}{3 c^2 R^2} in their equations of motion. No such rigid rotation applies to the exterior, where the field is non-uniform.^[7]

Observable Effects

Gyroscope Precession

Frame-dragging induces a precession in the spin axis of a gyroscope, known as the Lense-Thirring precession, which arises from the gravitomagnetic field generated by a rotating mass. This effect causes the gyroscope's angular momentum vector to precess around the angular momentum vector of the central body at a rate given by

\vec{\Omega}_{LT} = \frac{G I \omega}{c^2 r^3} \left[ 3 (\hat{r} \cdot \hat{\omega}) \hat{r} - \hat{\omega} \right],

where G is the gravitational constant, I is the moment of inertia of the rotating body, \omega is its angular speed, c is the speed of light, r is the distance from the center of the rotating body, and \hat{r} and \hat{\omega} are the unit vectors in the directions of the position and angular velocity, respectively.^[21]^[22] This Lense-Thirring precession must be distinguished from other relativistic spin precessions, such as the de Sitter (geodetic) precession, which results from the curvature of spacetime due to the mass alone, and the Thomas precession, a special relativistic effect from the non-commutativity of boosts for a spinning particle in accelerated motion. The frame-dragging component specifically originates from the gravitomagnetic interaction, proportional to the rotation of the central body.^[23] For an Earth-based gyroscope, the predicted Lense-Thirring precession due to Earth's rotation is approximately 0.041 arcseconds per year, highlighting the minuscule scale of the effect that requires high-precision instruments for detection.^[24] In the context of orbiting gyroscopes, frame-dragging also manifests as a nodal precession of the orbital plane, with a secular rate of

\dot{\Omega} = \frac{2 G J}{c^2 a^3 (1 - e^2)^{3/2}},

where J = I \omega is the angular momentum of the central body, a is the semi-major axis, and e is the eccentricity; this provides an analogous observable for testing the effect on extended spinning systems.^[25]

Orbital Frame-Dragging

Frame-dragging induces perturbations in the orbits of satellites around a rotating central body, manifesting primarily as a secular advance in the longitude of the ascending node, \Omega, due to the gravitomagnetic field generated by the body's angular momentum. This effect, known as the Lense-Thirring nodal precession, causes the orbital plane to be dragged in the direction of the body's rotation. The theoretical prediction for this secular rate is given by

\dot{\Omega} = \frac{2 G J}{c^2 a^3 (1 - e^2)^{3/2}},

where G is the gravitational constant, J is the angular momentum of the central body, c is the speed of light, a is the semi-major axis of the orbit, and e is the orbital eccentricity.^[25] In addition to nodal precession, frame-dragging contributes a smaller perturbation to the argument of perigee, \omega, which represents a shift in the orientation of the orbital ellipse within the plane. This gravitomagnetic contribution to the perigee advance is

\dot{\omega} = -\frac{6 G J \cos i}{c^2 a^3 (1 - e^2)^2},

where i is the orbital inclination. Unlike the dominant geodetic precession arising from spacetime curvature, the frame-dragging term for perigee shift is typically an order of magnitude smaller and opposite in sign for prograde orbits.^[25] The frame-dragging signal in satellite orbits couples strongly with classical perturbations from the Earth's oblateness, parameterized by the J_2 term in its gravitational multipole expansion. The J_2 effect produces a much larger nodal regression, on the order of degrees per year for low-Earth orbits, necessitating highly accurate modeling of even zonal harmonics and their uncertainties to isolate the gravitomagnetic component. For low-Earth polar orbits, such as those of the LAGEOS satellites, the predicted frame-dragging nodal precession is approximately 30-40 milliarcseconds per year, providing a measurable scale for general relativity tests despite the tiny magnitude relative to Newtonian effects.^[26]

Experimental Confirmation

Ground-Based Tests

Ground-based tests of frame-dragging face significant challenges due to the minuscule magnitude of the gravitomagnetic effects generated by laboratory-scale rotating masses or Earth's rotation, which are orders of magnitude weaker than Newtonian gravitational forces. These effects demand detectors with sensitivities approaching 10^{-14} rad/s or better to distinguish the signal from environmental noise, seismic vibrations, and classical electromagnetic or mechanical torques that can mimic or contaminate the measurement. Ultra-high vacuum, cryogenic cooling, and mechanical isolation are essential to achieve such precision, but even then, null results or tight upper limits are typical, providing valuable constraints on general relativity in the weak-field regime. Similar cryogenic setups with rotating superconductors, such as niobium rings cooled to liquid helium temperatures and spun at high angular velocities, were later used to search for frame-dragging-like signals with accelerometers and laser gyroscopes; observed effects were below detection thresholds after accounting for systematics, confirming no anomalous gravitomagnetic coupling beyond predicted levels.^[27] Theoretical proposals for future ground tests include using superconducting gravimeters to detect time-varying gravitomagnetic signals from Earth's rotation or local sources, leveraging their high stability (noise levels below 10^{-9} g/√Hz) to isolate frame-dragging-induced perturbations in the gravitational potential. These instruments could provide complementary constraints to space-based measurements by focusing on low-frequency signals, though realization requires further advances in noise suppression and signal modeling to overcome the inherent weakness of the effect.^[28]

Space Mission Results

The Gravity Probe B (GP-B) mission, launched by NASA in 2004 and operational until 2011, provided a direct measurement of frame-dragging through the precession of ultra-precise gyroscopes in a polar Earth orbit at an altitude of approximately 640 km. The experiment detected the frame-dragging effect as a drift in the gyroscope spin axes at a rate of -37.2 ± 7.2 milliarcseconds per year, compared to the general relativistic prediction of -39.2 milliarcseconds per year, confirming the effect to within 19% accuracy after extensive data analysis to account for classical torques and electrostatic disturbances. This result marked the first space-based verification of frame-dragging using gyroscopic precession, demonstrating the dragging of local inertial frames by Earth's rotation. Laser ranging observations of the LAGEOS I and II satellites, launched in 1976 and 1992 respectively, have been used to measure the Lense-Thirring nodal precession induced by frame-dragging on their orbits. In a 2004 analysis of data spanning 1998 to 2002, the measured precession rate was found to be 99 ± 5% of the general relativistic prediction after corrections for the dominant J2 oblateness perturbation using the Earth's gravity model. A subsequent 2016 reanalysis incorporating improved multipole gravity models reduced systematic errors from even zonal harmonics, confirming the nodal precession to within approximately 10% of the predicted value.^[26] The LARES (Laser Relativity Satellite) mission, launched in 2012 by the Italian Space Agency, complemented LAGEOS observations by providing a third laser-ranged satellite in a complementary orbit to further constrain gravitational modeling errors. Combining about 3.5 years of LARES data with LAGEOS I and II observations from 2012 to 2015, the frame-dragging effect was measured with a residual uncertainty of around 2%, yielding a gravitomagnetic field value of (1.93 ± 0.35) × 10^{-14} s^{-2}, consistent with general relativity within 2.5 standard deviations after accounting for 4% systematic errors from Earth's even zonals. This improved the overall precision of Earth-orbit frame-dragging tests by minimizing uncertainties in the geopotential. Analyses up to 2019, utilizing seven years of laser-ranged data from LARES, LAGEOS I, and LAGEOS II (2011–2018), further refined the measurement, recovering the Lense-Thirring precession with an uncertainty of about 2% through enhanced modeling of non-gravitational perturbations and GRACE-derived gravity fields.^[29] The LARES 2 mission, launched in July 2022, aims to achieve even higher precision. First results from 434 days of data, reported in 2023, confirm frame-dragging in complete agreement with general relativity predictions, with a combined nodal shift of approximately 61.36 milliarcseconds per year for LARES 2 and LAGEOS satellites. The preliminary analysis shows excellent consistency, with projected accuracy of a few parts in one thousand (<0.1%) expected after about three years of observations, once tidal effects are fully mitigated.^[30] These space mission results collectively establish frame-dragging as a verifiable prediction of general relativity, with accuracies improving from 19% in gyroscope-based tests to 1–2% in early orbital measurements and ongoing refinements toward sub-0.1% with LARES 2.

Astrophysical Evidence

Solar System Measurements

Lunar laser ranging (LLR), initiated with retroreflectors placed on the Moon by Apollo missions in the 1970s and continuing to the present, has yielded constraints on solar frame-dragging through analysis of perturbations in the lunar orbit caused by the Sun's rotation. Early analyses in the 1990s, using LLR data to fit the Earth-Moon system's dynamics, limited deviations from general relativity's gravitomagnetic predictions to less than 10% of the expected Lense-Thirring effect, confirming consistency with GR within that bound.^[31]^[32] More recent LLR observations have tightened these constraints, placing upper limits on gravitomagnetic departures from GR at the 0.15% level by modeling range signatures at synodic frequencies induced by the Earth-Moon barycenter's motion in the solar gravitomagnetic field.^[33] Planetary ephemerides, such as INPOP and DE430, incorporate Lense-Thirring terms to model frame-dragging perturbations from the Sun's angular momentum on inner planet orbits, particularly Mercury and Venus. These ephemerides are fitted using extensive observations including radio ranging from spacecraft like Messenger and Venus Express. Analyses in the 2020s, using INPOP19a, confirm the solar Lense-Thirring effect to within approximately 20% of GR predictions by adjusting the Sun's angular momentum parameter in the dynamical models, with residuals consistent with the expected perihelion advances of order 10^{-4} arcsec/century for Venus.^[34]^[25] The Cassini mission's radio science experiment during its 2002 superior conjunction (often referenced in conjunction with 2004 orbital data) measured the solar gravitomagnetic field through Doppler shifts in radio signals passing near the Sun, providing evidence for frame-dragging effects. Published results in 2011 interpreted these data as confirming the Lense-Thirring prediction to within 20%, distinguishing the rotational component from translational gravitomagnetic contributions via multi-frequency observations.^[35]^[36] Upper limits on frame-dragging deviations have also been derived from trajectories of asteroids and comets, incorporated into ephemerides like EPM2017 alongside planetary data. Observations of over 300 asteroids and several comets, processed with dynamical models including Lense-Thirring terms, rule out deviations from GR predictions exceeding 5%, as the fitted residuals for perihelion advances align with expected solar spin-induced perturbations at the level of 10^{-5} to 10^{-4} arcsec/century.^[37]^[38]

Observations of Compact Objects

Observations of frame-dragging in compact objects, such as neutron stars and black holes, provide crucial tests of general relativity in strong-field regimes. In binary systems containing neutron stars, pulsar timing measurements reveal precessional effects attributable to geodetic and frame-dragging contributions. For the double pulsar system PSR J0737−3039, discovered in 2003, long-term timing observations have tracked the orbital dynamics and spin precession, with analyses incorporating post-Newtonian models that confirm these effects to within a few percent accuracy, consistent with general relativity predictions including Lense-Thirring precession from the companions' angular momenta. These measurements distinguish frame-dragging from other relativistic effects by isolating the spin-dependent terms in the orbital dynamics.^[39] X-ray observations of accretion processes around compact objects further probe frame-dragging through spectral distortions. In systems with accreting black holes, the broadening of iron Kα emission lines arises from relativistic effects in the Kerr metric, including Doppler shifts, gravitational redshift, and frame-dragging near the innermost stable circular orbit. For instance, high-resolution X-ray spectroscopy has been used to measure black hole spin parameters by modeling these line profiles, where the asymmetric broadening encodes the dragging of spacetime by the rotating central object. For neutron stars, missions like NICER have applied pulse-profile modeling to X-ray hotspots, incorporating general relativistic effects such as light bending and gravitational redshift (but neglecting frame-dragging) in the spacetime metric around the rotating star PSR J0030+0451 to constrain its mass (1.34^{+0.15}{-0.16} M⊙) and radius (12.71^{+1.14}_{-1.19} km) at 68% confidence based on 2017–2018 data, with 2024 reanalyses yielding similar ~10% precision. For black holes, complementary X-ray missions like XMM-Newton have applied similar relativistic modeling to iron lines in sources like Cygnus X-1, yielding spin estimates up to a/M = 0.99 with frame-dragging signatures.^[40]^[41] Imaging of supermassive black holes by the Event Horizon Telescope (EHT) offers direct visual evidence of frame-dragging effects near event horizons. The 2019 image of M87* revealed an asymmetric shadow consistent with a rotating black hole, where the photon ring's lopsided brightness and the alignment of the relativistic jet with the spin axis indicate strong frame-dragging twisting the surrounding plasma. Subsequent 2022 observations of Sgr A* showed similar asymmetry in the shadow, with the jet direction (if present) and polarization patterns supporting spin-induced dragging, constraining the black hole's dimensionless spin to a/M ≈ 0.9 for M87* and placing upper limits on deviations from the Kerr metric. 2024 EHT results confirmed the persistent nature of the M87* shadow and magnetic field structures, further supporting frame-dragging signatures in the asymmetric emission. These features arise because frame-dragging shifts the photon orbits asymmetrically, with co-rotating photons experiencing enhanced orbital support.^[42] Gravitational wave detections from black hole mergers by LIGO and Virgo provide stringent constraints on frame-dragging in the ringdown phase. The post-merger signal's quasinormal modes, which describe the damped oscillations of the final black hole, encode the Kerr geometry's frame-dragging through their frequencies and damping times. Analyses of events from GW150914 (2015) through the third observing run (up to 2020) and beyond show no deviations from general relativity, with ringdown spectra matching predictions for spinning black holes to within a few percent, confirming the no-hair theorem and the role of angular momentum in spacetime dragging. For example, the dominant (2,2) mode in GW150914 implies a final spin of a/M ≈ 0.68, with subdominant modes further validating the linear perturbation theory in strong fields. Ongoing observations up to 2025 continue to tighten these bounds, ruling out alternative theories that alter frame-dragging at the percent level.

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[21]
The Thirring-Lense Papers 1
The collaboration of Lense and Thirring began in Vienna after Thirring, aware of Lense's background in astronomy, inquired whether Lense would be willing to ...
[22]
[PDF] PRECESSIONS IN RELATIVITY - arXiv
The Lense- Thirring precession frequency is ωLT=GI/2c²R³·[3R/R²(ω·R)-ω], where the vector R is the distance from the center of the rotating sphere, of radius r ...
[23]
GP-B — Spacetime & Spin - Gravity Probe B
Schiff ~1970, Drag-free motion. The drag-free control system is only one ... Gravitomagnetism is also thought to explain the generation of the astounding ...
[24]
[PDF] Geodetic Precession or Dragging of Inertial Frames?
In this paper it is shown that the geodetic precession of a gyroscope orbiting a spherically symmetric, nonrotating mass can by recast as a Lense-Thirring frame ...
[25]
[PDF] Phenomenology of the Lense-Thirring effect in the Solar System
Sep 30, 2010 · Thus, the gravitomagnetic field of the Earth contributes to the value of the second even zonal of the geopoten- tial retrieved from the orbital ...
[26]
[PDF] A test of general relativity using the LARES and LAGEOS satellites ...
Mar 4, 2016 · In. 2011 the dedicated space mission Gravity Probe B, launched in 2004 by NASA, reported also a test of frame-dragging with approximately 20 ...
[27]
Atom Interferometry tests of the isotropy of post-Newtonian gravity
Oct 19, 2007 · We present a test of the local Lorentz invariance of post-Newtonian gravity by monitoring Earth's gravity with a Mach-Zehnder atom interferometer.Missing: frame- dragging rotation
[28]
Testing gravity with cold atom interferometry: results and prospects
Atom interferometers have been developed in the last three decades as new powerful tools to investigate gravity.
[29]
An improved test of the general relativistic effect of frame-dragging ...
Oct 23, 2019 · We report the improved test of frame-dragging, an intriguing phenomenon predicted by Einstein's General Relativity, obtained using 7 years of Satellite Laser ...
[30]
[PDF] Lunar Laser Ranging - NASA
– captures the full “frame dragging” effect sought by GP-‐B (meas. to. 19%; 1 ... • The earth moving in the Solar System Barycenter (SSB) frame produces a.
[31]
[PDF] Lunar laser ranging: the millimeter challenge - UCSD Physics
Jun 14, 2013 · Lunar laser ranging (LLR) measures the Earth-Moon distance using laser pulses, now in the millimeter regime, to test gravity and planetary ...
[32]
Tests of Gravity Using Lunar Laser Ranging - PMC - PubMed Central
If another experiment claimed a gravitomagnetic, or “frame-dragging” departure from GR at even the 1% level, LLR data would stand in conflict [39]. Modeling ...
[33]
Testing theories of gravity with planetary ephemerides
Jan 29, 2024 · The Lense–Thirring effect hence depends on the Sun angular momentum, \varvec{S} that can be obtained by considering different models for the Sun ...
[34]
[PDF] arXiv:1002.4585v5 [gr-qc] 18 Jan 2011
Jan 18, 2011 · The Lense-Thirring effect of the Sun. Figure 36 shows the effect of the solar gravitomagnetic field on the Earth-Jupiter range. Its peak-to ...
[35]
Gravimagnetic effect of the barycentric motion of the Sun and ...
Jul 30, 2007 · Our analysis suggests that the translational gravimagnetic field of the Sun can be extracted from the Cassini data, and its effect is separable ...
[36]
Estimates of the change rate of solar mass and gravitational ...
The Lense-Thirring effect is especially important for the determination of the time-varying value of GM⊙ because it allows us to build a much more correct orbit ...
[37]
[PDF] Recent Attempts to Measure the General Relativistic Lense-Thirring ...
Nov 30, 2009 · Recent progresses in the planetary orbit determination make the perspective of reliably measuring the Sun's Lense-Thirring effect a realistic ...
[38]
A NICER View of PSR J0030+0451: Millisecond Pulsar Parameter ...
Dec 12, 2019 · We report on Bayesian parameter estimation of the mass and equatorial radius of the millisecond pulsar PSR J0030+0451, conditional on pulse-profile modeling.