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Large constellations of bright artificial satellites in low Earth orbit pose significant challenges to ground-based astronomy. Current orbiting constellation satellites have brightnesses between apparent magnitudes 4 and 6, whereas in the near-infrared Ks band, they can reach magnitude 2 (ref. ). Satellite operators, astronomers and other users of the night sky are working on brightness mitigation strategies. Radio emissions induce further potential risk to ground-based radio telescopes that also need to be evaluated. Here we report the outcome of an international optical observation campaign of a prototype constellation satellite, AST SpaceMobile's BlueWalker 3. BlueWalker 3 features a 64.3 m phased-array antenna as well as a launch vehicle adaptor (LVA). The peak brightness of the satellite reached an apparent magnitude of 0.4. This made the new satellite one of the brightest objects in the night sky. Additionally, the LVA reached an apparent V-band magnitude of 5.5, four times brighter than the current International Astronomical Union recommendation of magnitude 7 (refs. ); it jettisoned on 10 November 2022 (Universal Time), and its orbital ephemeris was not publicly released until 4 days later. The expected build-out of constellations with hundreds of thousands of new bright objects will make active satellite tracking and avoidance strategies a necessity for ground-based telescopes.
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http://www.ncbi.nlm.nih.gov/pmc/articles/PMC10686822 | PMC |
http://dx.doi.org/10.1038/s41586-023-06672-7 | DOI Listing |
Sci Adv
September 2025
School of Physical and Chemical Sciences, University of Canterbury, Christchurch 8140, New Zealand.
High-precision, Sagnac interferometry has long been proposed as a route to test fundamental questions in physics such as the magnitude of relativistic precessions (e.g., the Lense-Thirring effect).
View Article and Find Full Text PDFSensors (Basel)
July 2025
Beijing Research Institute of Telemetry, China Aerospace Science and Technology Corporation, Beijing 100094, China.
High-precision time-frequency systems are essential for low Earth orbit (LEO) navigation satellites to achieve real-time (RT) centimeter-level positioning services. However, subject to stringent size, power, and cost constraints, LEO satellites are typically equipped with oven-controlled crystal oscillators (OCXOs) as the system clock. The inherent long-term stability of OCXOs leads to rapid clock error accumulation, severely degrading positioning accuracy.
View Article and Find Full Text PDFUnder dynamic conditions, star spots will move on the image plane of the star sensor, resulting in trailing of the star map. This trailing can significantly reduce the accuracy of star centroid positioning, thereby affecting satellite attitude determination. Unlike traditional methods that restore blurred star maps before positioning, we treat the centroid of the star point as a key point in the trailing star map and use a deep learning model based on object detection to convert the positioning of star points under dynamic conditions into the positioning of key points in the trailing star map.
View Article and Find Full Text PDFAtmospheric scattering occurs over a horizontal scale of several kilometers. This results in influence from neighboring surface features on the signal recorded over a given position, reducing contrast and the accuracy of quantitative retrievals of surface reflectance from satellite imagery. This atmospheric blurring, or adjacency effect, must be accounted for when both contrast in surface reflectance and magnitude of atmospheric scattering are significant.
View Article and Find Full Text PDFJ Opt Soc Am A Opt Image Sci Vis
February 2025
The guide star catalog plays a crucial role in the star sensor, impacting the system's star identification speed and attitude measurement accuracy. Currently, the generation method for the guide star catalog is well developed for star sensors used on satellites. However, the inter-FOV guide star catalog for the all-time three-FOV star sensor still faces challenges such as excessive storage requirements, non-uniform distribution of guide stars, and incompleteness.
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