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XPoSat

The X-ray Polarimeter Satellite (XPoSat) is an Indian space-based observatory developed by the Indian Space Research Organisation (ISRO) to measure the polarization of cosmic X-rays from bright astronomical sources, marking the country's first dedicated mission in X-ray polarimetry.^[1] Launched on January 1, 2024, aboard a Polar Satellite Launch Vehicle (PSLV-C58) from the Satish Dhawan Space Centre, the 469 kg spacecraft was placed into a low Earth orbit at approximately 650 km altitude with a 6° inclination.^[2] With a nominal mission lifespan of five years, XPoSat aims to provide insights into high-energy astrophysical processes, including the geometry of emission regions near black holes and the magnetic field configurations in extreme environments such as supernova remnants and active galactic nuclei jets.^[1] XPoSat carries two primary scientific payloads: the Polarimeter Instrument in X-rays (POLIX) and the X-ray Spectroscopy and Timing (XSPECT) payload. POLIX, developed by the Raman Research Institute, operates in the 8–30 keV energy band using Thomson scattering to measure the degree and angle of polarization for about 50 bright X-ray sources, enabling studies of accretion dynamics around compact objects and tests of general relativity in strong gravitational fields.^[2] Complementing this, XSPECT, built by the U. R. Rao Satellite Centre, functions in the softer 0.8–15 keV range to deliver high-resolution spectroscopy (better than 200 eV at 6 keV) and timing information, facilitating simultaneous multi-wavelength observations with missions like AstroSat.^[3] Since its successful deployment, XPoSat has achieved key milestones, including polarization measurements from the Crab pulsar and black hole binaries such as Cygnus X-1, contributing to global X-ray astronomy by filling a gap in medium-energy polarimetry capabilities. As of November 2025, the mission remains fully operational, with data publicly available through ISRO's Indian Space Science Data Centre (ISSDC) for international scientific collaboration. In October 2025, ISRO released the first tranche of scientific data from the mission to the public.^[4]^[5]

Mission Overview

Objectives

The primary objective of the XPoSat mission is to measure the polarization degree and angle of X-rays emanating from approximately 50 bright astronomical sources, including black hole binaries, neutron stars, and pulsars, within the energy band of 8-30 keV.^[6]^[2] This polarimetry capability aims to probe the physical processes in these extreme environments by revealing the orientation and alignment of X-ray emissions.^[6] A secondary goal is to conduct simultaneous spectroscopy and timing observations in the 0.8-15 keV range, providing complementary data to the polarimetric measurements for a more complete analysis of source properties.^[2] These instruments, POLIX for polarimetry and XSPECT for spectroscopy and timing, enable the mission to achieve these objectives through coordinated observations.^[6] Broader scientific aims include elucidating emission mechanisms, the geometry of accretion disks, and the configuration of magnetic fields in high-energy astrophysical phenomena, while facilitating long-term monitoring of X-ray source variability to track evolutionary changes.^[2]^[6] The mission is designed for a minimum operational duration of five years to support extended studies of these dynamic sources.^[1]

Spacecraft Design

The XPoSat spacecraft has an overall mass of 469 kg at launch. This configuration allows for efficient deployment in low Earth orbit while accommodating the necessary subsystems for long-duration operations. The satellite is built on a modified IMS-2 bus platform, which provides a reliable architecture derived from ISRO's established microsatellite heritage for scientific missions.^[7]^[8]^[9] Key features of the bus design include deployable solar panels capable of generating approximately 850 W of power to support all onboard systems, four reaction wheels for attitude control, and star trackers that enable precise pointing accuracy better than 1 arcmin. The power subsystem incorporates lithium-ion batteries for energy storage during eclipse periods, while thermal control is maintained through dedicated heaters to ensure instrument stability in varying orbital thermal environments. Additionally, specialized radiation shielding protects the X-ray-sensitive components from cosmic radiation effects. These elements collectively ensure robust performance in the demanding space environment.^[10]^[8] Data handling is facilitated by an onboard storage capacity of 128 GB for science and housekeeping data, with telemetry transmitted via S-band at 2 kbps for command and monitoring, and high-rate science data downlinked through X-band at up to 8 Mbps during ground station passes. The attitude control strategy begins with spin stabilization immediately post-separation to provide initial stability, transitioning to three-axis stabilization using the reaction wheels and thrusters for fine pointing during targeted observations. This design supports the seamless operation of the POLIX and XSPECT payloads by maintaining optimal orientation and data integrity throughout the mission.^[8]^[10]

Development and Launch

Development History

The XPoSat mission originated from efforts by the Raman Research Institute (RRI) and ISRO's U R Rao Satellite Centre (URSC) to develop capabilities in X-ray polarimetry, with full-fledged project initiation occurring in 2015 through a formal agreement between ISRO and RRI.^[11] The proposal aimed to create India's first dedicated satellite for measuring X-ray polarization from cosmic sources, building on prior ground-based research in the field. In September 2017, ISRO formally approved the project and provided an initial grant of ₹95,000,000 to support early-phase activities, with the total mission budget allocated at approximately ₹250 crore (US$30 million).^[12]^[13] Key collaborators included RRI, which led the design and fabrication of the primary POLIX polarimeter payload, and URSC, responsible for the XSPECT spectroscopy and timing instrument as well as overall spacecraft integration.^[5] The Inter-University Centre for Astronomy and Astrophysics (IUCAA) contributed science support, facilitating proposal development, data analysis workshops, and user training for the mission's observational program.^[14] These partnerships leveraged expertise in X-ray instrumentation and astrophysics to address the technical demands of polarimetry in space. Development progressed through key milestones, including the Preliminary Design Review (PDR) for the spacecraft and POLIX payload completed by September 2018, which validated the core architecture.^[12] Prototype testing and qualification model development followed from 2018 to 2020, focusing on instrument performance in the 8-30 keV energy range for POLIX. Integration of payloads with the satellite bus occurred between 2021 and 2023, culminating in full spacecraft assembly in 2022. Challenges in calibrating the POLIX scatterer for accurate polarization measurements were overcome using ground-based simulations and X-ray beam tests to model response and minimize systematic errors.^[15] Pre-launch preparations intensified in late 2023 at URSC, where the satellite underwent comprehensive vibration, acoustic, and thermal vacuum testing to simulate launch and orbital environments, confirming structural integrity and operational reliability prior to integration with the PSLV-C58 launch vehicle.^[16] These phases ensured the mission's readiness for deployment, marking a significant advancement in India's space-based X-ray astronomy capabilities.

Launch Sequence

The XPoSat mission lifted off on January 1, 2024, at 09:10 IST from the First Launch Pad at Satish Dhawan Space Centre, Sriharikota, aboard the Polar Satellite Launch Vehicle (PSLV-C58) in its DL configuration, featuring four solid strap-on boosters.^[8]^[7] The launch sequence proceeded nominally with the ignition of the PSLV's first stage at liftoff, providing initial ascent through its solid propellant core and strap-ons, reaching an altitude of approximately 24 km at strap-on separation after 70 seconds. Subsequent stages ignited sequentially: the second stage liquid engine propelled the vehicle beyond 100 km, the third stage solid motor extended the trajectory, and the fourth stage liquid engine performed the final burn, culminating in cutoff at T+1259 seconds at an altitude of 650 km and velocity of 7529 m/s. XPoSat, weighing 469 kg, separated from the fourth stage at T+1316 seconds (approximately 22 minutes after liftoff), achieving injection into a low Earth orbit of 650 km altitude and 6° inclination. Following XPoSat's deployment, the fourth stage was maneuvered for the release of 10 co-passenger payloads under the PSLV Orbital Experimental Module-3 (POEM-3) initiative.^[7]^[17] The PSLV-C58 demonstrated high precision in payload injection, with orbital parameters deviating by only about 3 km from the targeted values, resulting in a near-circular orbit suitable for the mission's observational requirements. Post-separation, XPoSat's solar arrays deployed successfully, enabling onboard power generation. Telemetry signals were promptly acquired by ISRO's Master Control Facility and tracking stations, with initial systems health checks confirming nominal performance across all subsystems within hours of launch.^[8]^[18]^[19]

Orbit and Operations

Orbital Configuration

XPoSat operates in a low Earth orbit (LEO) at an altitude of approximately 650 km with a circular configuration and an inclination of 6° relative to the equator. This near-equatorial orbit was achieved following injection by the PSLV-C58 launch vehicle.^[7]^[20] The satellite maintains three-axis stabilization to enable precise pointing toward celestial X-ray sources. This configuration supports targeted observations lasting 30 to 90 minutes per orbital pass, during which the spacecraft rotates around its viewing axis at about 0.2 RPM to measure polarization at varying azimuthal angles.^[7]^[2] Given its low-inclination orbit, XPoSat transits the South Atlantic Anomaly (SAA) approximately every orbit, exposing it to elevated particle flux and radiation levels. To mitigate potential damage to sensitive detectors, both primary instruments—POLIX and XSPECT—are automatically shut off during SAA passages, limiting operational exposure while adhering to radiation dose constraints for long-term reliability.^[21] The orbit is subject to gradual decay due to atmospheric drag, with the mission designed for a nominal lifetime of 5 years, after which natural orbital decay is anticipated.^[6]

Mission Timeline

Following its launch on January 1, 2024, aboard the PSLV-C58 rocket from the Satish Dhawan Space Centre, the XPoSat spacecraft entered its activation phase shortly thereafter.^[8] The XSPECT instrument was switched on January 2, 2024, initiating the Performance Verification (PV) phase, which included system checks, calibration validation, and initial pointing tests.^[22] First source observations by XSPECT began on January 5, 2024, targeting Cassiopeia-A, followed by additional PV-phase observations of sources like Tycho, the Crab pulsar, and GX 301-2. The POLIX instrument underwent similar commissioning, with its first pointing tests and observations of the Crab pulsar conducted between January 15 and 18, 2024, completing the initial activation and commissioning by mid-January.^[23]^[22] Routine scientific operations commenced in February 2024, following the successful PV phase, with both instruments fully activated for ongoing data collection.^[23] The first year of operations emphasized observations of priority sources, enabling detailed polarimetry and spectroscopy studies of bright X-ray emitters.^[6] Approximately 60% of the observing time was allocated to guest observers through the Announcement of Opportunity (AO) process, primarily for XSPECT-based proposals, fostering broader scientific participation from the Indian community.^[24] A key milestone occurred on October 13, 2025, when ISRO released the first public datasets from the mission, totaling 143 GB, during a national meet organized to share scientific data and tools via the Indian Space Science Data Centre (ISSDC) portal.^[5] On the same day, the first AO cycle was announced, inviting proposals from Indian scientists for XSPECT observations, with submissions due by November 30, 2025, to be evaluated by the XPoSat Time Allocation Committee (XTAC).^[24]^[25] The nominal mission duration is five years, with potential extensions beyond this period contingent on remaining fuel reserves, and plans for additional AO cycles to sustain long-term observations.^[6]

Instruments

POLIX

The POLIX (Polarimeter Instrument in X-rays) is a Thomson scattering-based X-ray polarimeter designed to measure the degree and angle of polarization from cosmic sources in the 8–30 keV energy band. The instrument features a central low-Z scatterer made of lithium-loaded plastic or beryllium, surrounded by four position-sensitive multi-wire proportional counters to detect scattered photons preferentially perpendicular to the incident polarization direction. Each detector consists of 12 anode cells for azimuthal localization and operates with a gas mixture of 90% xenon, 9% argon, and 1% methane at 800 Torr, providing position resolution of approximately 2 cm via charge division. A collimator limits the field of view to 3° × 3° to reduce off-axis background while maintaining sensitivity to point sources.^[26]^[27]^[28] Prior to integration, POLIX underwent comprehensive ground calibration at the Raman Research Institute using polarized X-ray beams from laboratory sources to verify its polarimetric response. Spectral calibration employed radioactive isotopes such as ^{55}Fe (emitting at 6 keV with ~25% FWHM resolution) and ^{109}Cd (22.1 keV line with ~30% FWHM), confirming energy-dependent performance across the band. The modulation factor, quantifying the instrument's ability to distinguish polarized signals, was measured at ~40% at 10 keV, with additional validation through Monte Carlo simulations mimicking scatterer rotation to account for the satellite's spin-induced modulation. These tests ensured accurate reconstruction of polarization parameters without on-orbit adjustments.^[26]^[15] During operations, POLIX collects scattered photon events over extended pointings spanning multiple orbits to accumulate sufficient statistics for polarization analysis, as the technique demands high flux for reliable measurements. The satellite's rotation at ~0.2 rpm around the boresight axis effectively modulates the scattering geometry, enabling phase-resolved polarimetry. Background is mitigated via integrated veto layers in the detectors for anti-coincidence rejection of charged particles and cosmic rays, achieving low noise levels suitable for faint sources. The effective collecting area is ~640 cm² at nominal energies around 15 keV, supporting efficient photon gathering within the constrained field of view.^[26]^[28] POLIX demonstrates strong performance for bright X-ray sources, with sensitivity to detect polarization degrees of ~5% in approximately 3 days of observation for Crab-like objects (flux ~1 Crab in the 8–30 keV band), based on minimum detectable polarization calculations for exposures around 250 ks. This capability stems from the instrument's optimized geometry and low background, allowing robust mapping of polarization variations. POLIX contributes directly to the mission's goal of elucidating emission geometries in accreting systems by providing simultaneous polarimetric data.^[27]^[28]

XSPECT

The XSPECT (X-ray Spectroscopy and Timing) instrument on XPoSat is designed for non-imaging spectroscopy and timing observations in the soft X-ray band, utilizing an array of 16 swept charge devices (SCDs) as detectors behind co-aligned collimators. The SCDs, each with a geometric area of approximately 4 cm², are grouped into four quad modules to provide a total effective collecting area exceeding 30 cm² at 6 keV, enabling measurements across an energy range of 0.8–15 keV with a timing resolution of ~2 ms.^[29]^[3] The collimators include seven units with a 3° × 3° field of view and eight with a 2° × 2° field of view, ensuring alignment with the spacecraft's pointing axis for targeted source observations.^[29] In-flight calibration of XSPECT was performed shortly after launch, with verification observations of the Crab Nebula conducted in January 2024 to confirm its performance parameters. These tests yielded an energy resolution better than 200 eV at 6 keV and an effective area of approximately 40 cm² at lower energies, aligning closely with pre-launch ground calibrations that anticipated better than 200 eV resolution at 6 keV. As of October 2025, in-flight performance remains consistent with specifications following data release.^[22]^[1]^[5] XSPECT operates in tandem with the POLIX instrument, providing simultaneous soft X-ray data that complements polarimetry measurements for multi-faceted source analysis. It supports extended monitoring campaigns, with exposure times up to 1 Ms, facilitating detailed spectral fitting to model emission features and the generation of high-time-resolution light curves for variability studies.^[22]^[29] The instrument's design ensures pile-up-free operation for source fluxes up to 1 Crab unit, allowing reliable spectroscopy of bright X-ray emitters without distortion from event overlap. XSPECT is capable of detecting key emission lines, such as the iron K-alpha line at 6.4 keV, which is crucial for probing plasma conditions in astrophysical environments like accretion disks and supernova remnants.^[22]

Scientific Observations

Initial Observations

Following the successful launch and initial commissioning phase, the XSPECT instrument on XPoSat achieved first light by observing the Cassiopeia A supernova remnant on January 5, 2024. This performance verification observation, conducted over multiple orbits with a total integration time of 20 kiloseconds, detected prominent emission lines in the X-ray spectrum from elements including magnesium (Mg), silicon (Si), sulfur (S), calcium (Ca), and iron (Fe).^[3] The data also captured contributions from the Galactic cosmic ray background and cosmic X-ray background above 8 keV, validating XSPECT's spectroscopic capabilities in the 0.8–15 keV energy range.^[3] Commissioning of the POLIX instrument proceeded with initial polarization scans centered on the Crab Pulsar starting around January 10, 2024, and extending through observations from January 15–18, 2024. These scans produced a pulse profile matching expected characteristics, thereby confirming the instrument's baseline performance for X-ray polarimetry in the 8–30 keV band without significant deviations.^[23] In the ensuing first year, XPoSat targeted approximately 10 bright X-ray sources selected for early observations, encompassing categories such as black hole binaries, X-ray pulsars, low-mass X-ray binaries, and isolated neutron stars. Observations employed a pointing mode with 30–60 minute exposures per orbit, accumulated during the satellite's transit through Earth's shadow to minimize solar interference.^[3]^[6] Initial datasets from these observations were processed for instrument calibration, yielding high-quality spectra and polarimetric profiles suitable for scientific analysis. No major anomalies were reported in the payload operations or data telemetry during this phase.^[30]^[23]

Key Results

XSPECT observations identified a thermonuclear X-ray burst from 4U 1608-52 on March 19, 2025, characterized by a Type-I burst duration of about 15–20 seconds, followed approximately 16 minutes later by a superburst lasting roughly 3 hours.^[31] This event offers insights into nuclear ignition on the neutron star surface, with the burst's properties indicating rapid energy release from accumulated accreted material.^[31] In its first year of operations, XPoSat conducted observations of approximately 10 diverse high-energy sources, uncovering significant variability patterns in low-mass X-ray binaries (LMXBs).^[3] No solar observations were performed, as the mission focuses exclusively on galactic and extragalactic cosmic X-ray sources. These studies enhance understanding of wind accretion dynamics and transient behaviors in compact object systems.^[6] On October 13, 2025, ISRO publicly released 143 GB of mission data, facilitating broader community analysis and future discoveries in high-energy astrophysics.^[5]

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