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WorldView-3

WorldView-3 is a operated by (formerly ), launched on August 13, 2014, at 18:30:30 UTC from Vandenberg Air Force Base in aboard an 401 launch vehicle. It operates in a at an altitude of 617 km with a 98° inclination and a local time on descending node of 13:30 hours, enabling frequent high-resolution imaging of Earth's surface. The satellite's primary instrument, the WorldView-3 Imager, captures imagery across 29 spectral bands, including panchromatic at 0.31 m resolution, eight multispectral bands at 1.24 m, eight short-wave (SWIR) bands at 3.7 m, and twelve Clouds, Aerosols, Vapors, Ice, and Snow (CAVIS) bands at 30 m, with a ground swath width of 13.1 km. Designed with a nominal service life of 7.25 years but expected to operate for 10-12 years, WorldView-3 achieves a revisit time of less than one day for most locations when collecting at 1 m ground sample distance (GSD). As of November 2025, WorldView-3 remains operational, with an extended end-of-life projected for December 2025. Its advanced sensor suite represents a milestone as the first multi-payload, super-spectral, high-resolution commercial satellite, enhancing capabilities beyond traditional visible and near-infrared imaging through SWIR for material identification and CAVIS for atmospheric correction. The satellite delivers geolocation accuracy better than 3.5 m CE90 without ground control points, supporting precise mapping and analysis. WorldView-3 supports a wide range of applications, including , , , and resource management, with particular strengths in detecting plumes, mapping minerals, counting , and assessing forest health. Its high-resolution data has been instrumental in time-sensitive scenarios, such as post-disaster damage assessment and in conflict zones, contributing to global datasets used by governments, NGOs, and commercial entities. As part of Maxar's constellation, it complements earlier satellites by expanding coverage and , enabling more detailed and actionable intelligence.

Design and capabilities

Instruments

WorldView-3 is equipped with the WV110 advanced imaging system, which integrates a panchromatic imager, an eight-band multispectral imager in the visible and near-infrared (VNIR) spectrum, an eight-band short-wave infrared (SWIR) imager, and the Clouds, Aerosols, Vapors, Ice, and Snow (CAVIS) instrument. These sensors enable high-resolution with capabilities for atmospheric correction and enhanced material identification. The panchromatic imager operates in a single band from 450 to 800 nm, providing 0.31 m at for detailed black-and-white imaging of surface features. The multispectral imager covers eight VNIR bands—coastal (400–450 nm), blue (450–510 nm), green (510–580 nm), yellow (585–625 nm), red (630–690 nm), (705–745 nm), near-IR1 (770–895 nm), and near-IR2 (860–1040 nm)—at 1.24 m resolution, supporting applications in vegetation analysis, mapping, and coastal monitoring. The SWIR imager features eight bands spanning 1195–2365 nm (SWIR-1: 1195–1225 nm, SWIR-2: 1550–1590 nm, SWIR-3: 1640–1680 nm, SWIR-4: 1710–1750 nm, SWIR-5: 2145–2185 nm, SWIR-6: 2185–2225 nm, SWIR-7: 2235–2285 nm, SWIR-8: 2295–2365 nm), delivering 3.7 m and enabling imaging through atmospheric , , and aerosols for mineral exploration and environmental assessment. This SWIR capability provides unique atmospheric correction by distinguishing surface reflectance from atmospheric interference. The CAVIS instrument collects atmospheric data across 12 bands in the , visible, and SWIR spectra (e.g., desert clouds at 405–420 nm, aerosols at 459–509 nm and 2100–2250 nm, at 1620–1680 nm, at 930–965 nm), at 30 m , to correct imagery for obscurants like clouds, aerosols, and vapors. It operates simultaneously with the primary imagers to enhance data consistency and accuracy in challenging conditions. These instruments are integrated on a Ball Aerospace BCP 5000 bus, derived from the platform, supporting pushbroom scanning with up to 35,000 pixels in panchromatic mode and data rates of 800–1200 Mbit/s via X-band downlink. This configuration allows for efficient collection and transmission, with bi-directional scanning and rapid retargeting within seconds.

Imaging specifications

WorldView-3's imaging system delivers high-resolution panchromatic imagery at 0.31 meters (GSD) at , which is commercially sharpened to 0.30 meters through with multispectral . The multispectral visible and near- (VNIR) bands provide 1.24 meters GSD, while the short-wave (SWIR) bands offer 3.7 meters GSD, and the Clouds, Aerosols, , Ice, and Snow (CAVIS) instrument achieves 30 meters GSD for atmospheric monitoring. These resolutions enable detailed feature identification, from urban infrastructure to compositions, across a 13.1 km swath width at for panchromatic, multispectral, and SWIR imaging. The CAVIS bands support global coverage over time by providing atmospheric correction aligned with the primary swath. The satellite's revisit time is less than one day for most locations at 1-meter GSD, allowing rapid tasking and frequent monitoring of dynamic areas. It supports data collection modes such as stereo imaging for 3D modeling and multi-temporal acquisitions for change detection, with geolocation accuracy of 3.5 meters CE90 without ground control points. Spectral coverage spans the panchromatic band from 450 to 800 nm, enabling high-contrast black-and-white imagery. The eight multispectral VNIR bands include coastal (400–450 nm), blue (450–510 nm), green (510–580 nm), yellow (585–625 nm), red (630–690 nm), red edge (705–745 nm), near-infrared 1 (770–895 nm), and near-infrared 2 (860–1040 nm), facilitating applications in vegetation analysis and land cover classification. The eight SWIR bands cover 1195–1225 nm, 1550–1590 nm, 1640–1680 nm, 1710–1750 nm, 2145–2185 nm, 2185–2225 nm, 2235–2285 nm, and 2295–2365 nm, ideal for detecting hydrocarbons and mineral alterations. CAVIS includes 12 bands from 405 to 2250 nm for aerosol and cloud property assessment.
Imaging ModeResolution (m at nadir)Swath Width (km)Number of BandsKey Spectral Range (nm)
Panchromatic0.31 (sharpened to 0.30 commercially)13.11450–800
Multispectral (VNIR)1.2413.18400–1040
SWIR3.713.181195–2365
CAVIS3013.1 (global over time)12405–2250

Launch and mission

Launch details

WorldView-3 was launched on August 13, 2014, at 18:30 UTC (11:30 a.m. PDT) from Space Launch Complex 3E at Vandenberg Air Force Base in . The satellite served as the primary payload aboard a 401 rocket, configured with a 4-meter diameter for direct injection into a . The , provided through Commercial Launch Services, followed a near-polar trajectory, with the Centaur upper stage performing a primary burn lasting approximately 11 minutes after ignition at T+3:57, followed by a 3-minute coast phase and spin-up maneuver before payload deployment around T+19 minutes. Following separation, the underwent a rapid commissioning phase, with the fully activated and the main door opened by August 19, 2014. of the attitude determination and was completed on August 21, achieving initial operational capability shortly thereafter. The first images, captured over , , were acquired in late August 2014 and publicly released on August 27, demonstrating the satellite's advanced sensors. The launch and early operations proceeded nominally, with no significant anomalies reported during the initial mission phases.

Orbital parameters

WorldView-3 operates in a with a mean altitude of 617 km, an inclination of 97.9 degrees, and a of descending node at 13:30. This configuration provides consistent solar illumination across imaging passes, supporting reliable data collection for high-resolution . The 's is approximately 97 minutes, with an near 0, resulting in a nearly circular that minimizes variations in altitude and revisit patterns. The demonstrates high agility through control moment gyroscopes, enabling retargeting of 200 km on the ground in 12 seconds and slew rates supporting rapid pointing adjustments of several degrees per second. Designed with a minimum mission life of 7.25 years but extended through efficient fuel management, WorldView-3 has an expected end of life in December 2025, exceeding 11 years from launch. As of November 2025, the satellite remains operational. This longevity ensures sustained coverage capabilities over its operational span. The orbital parameters facilitate viewing geometry, which optimizes by aligning the directly overhead, while the sun-synchronous introduces seasonal variations in coverage, particularly at higher latitudes where angles affect accessible opportunities.

Operations and applications

Commercial operations

is operated by (formerly ), which provides high-resolution to government agencies, defense organizations, and private sector clients worldwide for applications in , , and . The enables commercial sales through tasked collection requests, where customers can order new acquisitions, and access to an extensive integrated with Maxar's broader constellation. products include panchromatic at 31 cm , multispectral bands at 1.24 m, and short-wave at 3.7 m, often delivered as sharpened 30 cm products; models for and tasked typically range from $24 to $36 per square kilometer for standard pan-sharpened bundles, varying by , coverage area, and processing level. A cornerstone of WorldView-3's commercial operations is its role in contracts with the U.S. (NGA) and (NRO), building on the EnhancedView program established in 2010. Imagery access transitioned to the Electro-Optical Commercial Layer (EOCL) contract awarded in 2022, a 10-year agreement that guarantees government access to WorldView-3 imagery alongside other satellites in the constellation for and purposes. WorldView-3 contributes to enhanced commercial offerings, such as 15 cm resolution mosaics created via Maxar's proprietary HD processing when integrated with data from complementary satellites like WorldView Legion, whose first satellites launched in 2024 with additional deployments in 2025. As of 2025, WorldView-3 remains in active service despite its age, with Maxar's overall archive encompassing over 11 billion square kilometers of cumulative high-resolution coverage across the constellation, enabling sustained revenue from imagery sales and subscriptions that bolster Maxar's leadership in the global geospatial market. The satellite's contributions to government contracts like EOCL have driven significant business impacts, including multi-hundred-million-dollar annual revenues and a dominant share of U.S. foundational geospatial intelligence provision.

Scientific and notable uses

WorldView-3 imagery has been instrumental in efforts, particularly for tracking in the region. Organizations such as the Amazon Conservation Association have utilized its high-resolution data to detect new deforestation hotspots through pre- and post-disturbance comparisons. The satellite's short-wave (SWIR) bands enhance health assessments by distinguishing non-photosynthetic components, such as stressed or degraded plant material, which is crucial for quantifying ; a 2019 study in tropical forests demonstrated that incorporating SWIR data improved classification accuracy for such features by up to 7.8%, aiding broader monitoring initiatives between 2015 and 2020. In , WorldView-3 provided critical sub-meter resolution imagery for assessing damage from the 2017 in . Researchers analyzed 0.5-meter WorldView satellite images from to map landslides and structural impacts, revealing over 40,000 slope failures across the island that informed recovery planning and hazard mitigation by federal agencies like the USGS. This enabled rapid identification of affected and loss, supporting efforts to prioritize in severely hit areas like the central mountainous regions. For urban and infrastructure monitoring, WorldView-3 has contributed to geopolitical analyses, such as tracking developments at North Korean missile sites in 2017. DigitalGlobe's WorldView-3 captured images of the following a detonation, revealing and tunnel collapses that indicated structural damage from the underground , as analyzed by experts for international assessments. Scientifically, WorldView-3's Clouds, Aerosols, Vapors, Ice, and Snow (CAVIS) instrument facilitates atmospheric corrections essential for climate studies, including mapping. The CAVIS bands, resembling MODIS channels, provide data on atmospheric constituents to refine surface reflectance estimates, enabling accurate analysis of haze-penetrated imagery; 's Commercial SmallSat has leveraged this for climate-related , confirming CAVIS quality sufficient for and vapor monitoring in peer-reviewed validations. Collaborations with have integrated CAVIS-corrected data into broader atmospheric models, supporting studies on global distribution and its climate impacts. Despite these applications, WorldView-3 data access is limited by U.S. regulations under the Kyl-Bingaman Amendment and NOAA licensing, which restrict high-resolution imaging over sensitive areas like foreign military installations to prevent potential risks; operators must apply limits or image shuttering in such zones, as relaxed in but still enforced for designated sites.

Technical specifications

Physical and power systems

The utilizes the Ball Aerospace BCP 5000 bus, a high-performance platform designed for advanced missions. The bus measures 5.7 meters in height and 2.5 meters in diameter, with a total span of 7.1 meters when the solar arrays are deployed. At launch, the had a total mass of 2,800 kg, encompassing the bus, , and propellants. The propulsion system employs a monopropellant configuration for attitude control and orbit maintenance, enabling precise maneuvers throughout the mission life. This system supports the satellite's requirements for station-keeping and momentum dumping, ensuring stable operations in its . is provided by dual solar arrays capable of generating up to 3.1 kW of electrical power during periods, supplemented by 100 Ah nickel-hydrogen batteries to sustain operations during orbital eclipses. The power subsystem is optimized for the satellite's high data rate demands and long-duration imaging sessions. Thermal control is achieved through a combination of passive radiators, multi-layer insulation, and active heaters, maintaining component temperatures within an operational range of -20°C to +50°C to protect sensitive electronics and instruments from the varying thermal environment in orbit. The avionics suite features a three-axis stabilized attitude determination and control system (ADCS), incorporating control moment gyroscopes (CMGs) for rapid slewing, star trackers (such as the Ball CT-602), a precision inertial reference unit (IRU), and GPS receivers for navigation. This configuration delivers sub-arcsecond pointing accuracy, enabling precise image acquisition with geolocation errors below 3.5 meters CE90 without ground control. Onboard solid-state storage provides 2.199 terabits of capacity with error detection and correction, supporting high-volume data handling.

Performance metrics

WorldView-3 was designed with a nominal mission life of 7.25 years but features an estimated extending 10 to 12 years, allowing for prolonged operations beyond its initial specifications. Launched on August 13, 2014, the satellite remains operational as of November 2025, with a planned end-of-life in December 2025, demonstrating extended reliability in its . The satellite's data downlink capabilities support high-volume image transmission via X-band at rates of 800 Mbit/s and up to 1200 Mbit/s for imagery and , enabling efficient delivery of high-resolution observations to ground stations. By 2025, WorldView-3 has contributed to the collection of extensive datasets as part of the Maxar constellation, with daily imaging capacity reaching approximately 680,000 km², supporting cumulative archives in the terabyte range over its operational lifespan. In terms of agility, WorldView-3 employs control moment gyros for rapid retargeting, achieving a slew of 200 km in just 12 seconds and supporting off-nadir imaging angles up to 20 degrees, which enhances its ability to capture dynamic scenes across wide areas. This maneuverability contributes to an average revisit time of less than one day for locations at 1 m resolution or better. Reliability is bolstered by redundant systems, including 3-axis stabilization with star trackers and GPS, resulting in no major in-orbit failures reported over more than a decade of service and pointing accuracy better than 500 m at image start and stop. The satellite's design emphasizes robust onboard storage of 2199 Gb with , ensuring consistent during operations. Key achievements include significant contributions to global basemaps and seamless integration within the Maxar constellation for high-resolution tasks. These efforts have supported diverse applications in mapping and monitoring while maintaining high operational uptime.

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