CCOR-2 (Compact CORonograph 2) is the second space coronograph of Compact Coronograph series. It is located aboard SOLAR-1 spacecraft placed at Lagrange 1 point – about 1.5 million kilometers (~930,000 miles) from the Earth towards the Sun. It will orbit the Sun at a distance between 0.974 and 1.006 AU.
It was launched in September 2025 from Florida.
Mission CCOR-2 will provide low latency, high cadence visible light images of solar corona and its surroundings. It will observe coronal mass ejections (CME) that are potentially dangerous to electronic infrastructure and because of that its data is going to be used for space weather forecasting.https://ccor.nrl.navy.mil/ccor1-inst-overview CCOR coronographs are descendants of aging SOHO/LASCO and STEREO/COR instruments.
It was primarily made for National Oceanic and Atmospheric Administration and Space Weather Prediction Center.
Launch and destination It was launched aboard SpaceX Falcon 9 Rocket from Kennedy Space Flight Center located on eastern Florida at 7:30 AM EDT on 24 September 2025.https://www.nrl.navy.mil/Media/News/Article/4313553/nrls-ccor-2-set-to-boost-space-weather-forecasting-capabilities/ It has reached L1 point on 23 January 2026 – that day its first light image was taken too.
Forecasting CCOR data (including CCOR-2) are used for space weather prediction. PyCAT (open source software designed by NOAA/SPWC and UK Met Office) and WSA-Enlil model are fed with coronograph data in order to perform calculations of CME mass, velocity and importantly – direction.https://nesdis-prod.s3.amazonaws.com/2025-11/Thernisien-CCORs-2025.pdf
Parameters and technical data
CCOR-2 was developed by US Naval Research Laboratory in Washington D.C.Space Weather Follow On (SWFO) Program Calibration and Validation Plan, SWFO-SYS-PLAN-0026, Revision A Space Weather Follow On (SWFO), Code 491.0, D. Vassiliadis, W. Rowland, C. Merrow, G. Comeyne, J. Carey, M. Honaker, et al. It has a length of about 72 centimeters (28.3 in) and its name highlights a small size of the instrument. It features a 2048×1920 pixels Active Pixel Sensor detector which detects wavelengths in the range of ~450 nm to ~750 nm.
The instrument has to follow several requirements, listed below.
A spatial resolution of ≤70 arcseconds Inner FOV geometric cutoff at 3.0 solar radii () Outer FOV at 20 or better A signal to noise ratio of 10 in the region between 4.4 and 22.7 (1.17° to 6.05°) Maximum image latency of 30 minutes CME mass estimate with an error of ≤50 per cent for CMEs with mass between kg and kg A closable outer door Full resolution image cadence of 15 minutes or 5 minutes for 2x2 binned images. Minimum signal intensity above noise of ( is solar surface brightness – about -10.6 mag/arcsec²) Coronal brightness measurement with error up to 10% CME velocity estimate with biggest allowed error of 5% in the range of 200 km/s to 3400 km/s At least five years of operations with resources enough for additional five years (requirement for entire spacecraft) CCOR-2 shall be able to meet all the requirements when observing during an X50 solar flare or S4 class solar storm Observing in visible light The data must be available for SWPC reach within 30 minutes of its creation CCOR shall be capable of surviving 5 years on orbit before start of operations
Actual specifications +Parameter ValueMass – entire instrumentMass of Power Supply BoxPower22.5 wattsPixel size10 µm × 10 µmDetector pixel array2048 by 1920 pixelsImaging pixels2038 by 1910 pixelsInner FOV geometric cutoff3.0 S/N ratio of ≥1 starting at3.5 Outer FOV (sides, diagonal)22.5 , 26.3 Resolution65 arcsecondsFOV with that resolution4 to 22 Focal length85.17 mmPlate scale24.27 arcseconds/pixelAmount of occulting disks (all glued together to form a single one) 24FWHM bandpass469 nm – 755 nmF-number5.32Cadence of full resolution images15 minutesLatency≤15 minutesData rate38.7 kbpsCCOR-2 images are available in FITS format, however they are processed do different data processing levels on the ground.
The first level of the images is L0 CCSDS which is a raw readout of detector pixels. L0 CCSDS is then rotated so solar north points upwards which creates a L0B file.
Level 1A image is formed using L0B file by converting DN value of pixel into Mean Solar Brightness unit, division by exposure time, correcting for vignetting and detector linearity rectification. It is the main operational product used for forecasting.
A median background is created from L1 by computing F-corona and stray-light based of the image. L1A with background subtraction, distortion correction application and flat field rectification creates L2 image.
CCOR-2 data is available to the public since 17 June 2026, 15 days after it passed its Provisional-maturity Product Validation Review.SOLAR-1/CCOR-2 Data Release
Provisional Data Quality
Read-Me for Data Users
Date: June 2, 2026
Version 1.0
Comet discoveries A small Kreutz sungrazer was found in the CCOR-2 coronograph images late on 29 June 2026. The discoverer of the object is Michael Stark.https://sungrazer.groups.io/g/SOHO/topic/120040259#msg6528 References
External links
Archive of CCOR-2 data Realtime data access Archive of CCOR-2 data and Read Me document