CNES GRACE/-FO Level 2A monthly unconstrained geopotential anomalies solutions






Description of the solutions
The GRACE and GRACE-FO missions
The GRACE (Gravity Recovery and Climate Experiment; Tapley et al., 2004; Tapley et al., 2019) and GRACE-FO (GRACE Follow-On; Chen et al., 2022; Landerer et al., 2020) satellite missions have, since 2002, provided monthly estimates of variations in the Earth’s gravity field and of mass redistributions on its surface or at depth. These redistributions include mass changes in ice sheets, movements of water masses linked to hydrological cycles, and displacements of mantle masses associated with glacial isostatic adjustment (GIA) and earthquakes. The GRACE and GRACE-FO missions consist of twin satellites equipped with a Star Camera Assembly (SCA), an accelerometer (ACC), GPS receivers, and K-band microwave transmitters (K-Band Ranging or KBR). The KBR data are processed as the relative velocity between the satellites, known as the K-Band Range-Rate (KBRR). These data are used to estimate Earth’s geopotential anomalies by inverting the normal equations generated by satellite orbit adjustments. This inversion yields the coefficients of the spherical harmonic decomposition of the geopotential, known as the Level 2A (L2A) solution. Within the framework of the unconstrained solution developed by CNES, classical inversion based on a Cholesky decomposition does not reduce the anisotropic noise in the solutions (see Lemoine et al., 2026 for more details). It is therefore necessary to apply Gaussian or DDK spatial filters (Kusche et al., 2009) to extract the geophysical signals of interest for Earth observation.
Files description
The time series of unconstrained GRACE CNES solutions is provided in the form of spherical harmonic coefficients up to degree and order 90, excluding degrees 0 and 1 (8,277 coefficients), as the GRACE and GRACE-FO satellites cannot estimate them accurately. These solutions are obtained through unconstrained inversion using a Cholesky decomposition (more details are available here). The solutions are distributed in ASCII files in the extended GRACE format, which is an extension of the original GRACE gravity model format (document GR-GFZ-FD-001 GRACE 327-732 (v1.1), November 27, 2003, available here). The coefficients are sorted in ascending order by degree and order. An example file is provided below.
Solution Quality Metrics
An initial assessment of the quality of the solutions can be found in the spectral amplitude of the coefficients. The GRACE/-FO satellites orbit the Earth approximately 15 times a day, so noise peaks are expected at degrees multiples of 15 (15, 30, 45, 60, …). This type of peak is an indicator of a noisier solution, as shown by the example of the 2025-11 solution illustrated in the figure below.

Due to the geometry of the GRACE/-FO satellites, the solutions have significant anisotropic noise that manifests as vertical stripes once converted to a grid (regardless of the unit), rendering the solution unusable in its current state. To reduce this noise, a filter must be applied to the harmonic coefficients. Generally, a DDK (Denoising Decorrelation Kernel) filter is applied to reduce noise, which decreases spatial resolution but makes the solution usable. You can find more details on the DDK filtering method here. Applying a DDK filter significantly reduces the amplitude of the spherical harmonic coefficients starting from a certain degree depending on the order of the DDK filter. Consequently, displaying the coefficients after applying the filter allows for the identification of abnormally high values, which are likely to generate anisotropic noise during the conversion of solutions to a grid, and provides a good estimate of the solution’s noise level. An example of a harmonic coefficient tree is shown below.

Using the solutions
In order to use these solutions, it is necessary to express the gravitational potential at every point on Earth. The Earth’s gravitational potential is expressed as follows:

Where r, φ and λ are, respectively, the radius, latitude, and longitude of the considered point, Cₙₘ and Sₙₘ re the harmonic coefficients of the solution, G es the universal gravitational constant, M eis the mass of the Earth, a is the Earth’s equatorial radius, P̄ₗₘ is the associated Legendre function of degree l and order m.
The solutions of the GRACE/-FO geopotential allow us to track variations in mass on the Earth’s surface, particularly water masses, since the solutions are generally expressed as variations in a thin layer of water on its surface. In this case, the previous equation becomes, when calculated up to a maximum degree Lₘₐₓ :

Où :
– ΔHᵂ(φ, λ) is the equivalent water height at latitude φ and longitude λ,
– a is the Earth’s average radius,
– ρᴱ is the average Earth density,
– ρʷ is the water density,
– kₗ is the Load Love Number (LLN) at any harmonic degree l,
– Ȳₗₘ are the Legendre polynomial functions for any degree l and order m, in complex notation
– ΔCₗₘ are the increments, relative to a reference gravitational solution, of the complex spherical harmonic coefficients of the solution.
More details about the method can be found in Ditmar (2018).
Dataset identifier
10.24400/170160/SAGSA_GGM_CHO_1MONTH_RL0005
Characteristics
| Product type | Stokes coefficients | |
| Format | ASCII files | |
| License | (CCBY) | |
| Start of production | GRACE: 01/04/2002 | GRACE-FO: 01/05/2018 | |
| End of production | GRACE: 01/05/2017 | GRACE-FO: Still producing | |
| Coverage | Global | |
| Coverage type | Spherical harmonics | |
| Spatial resolution | Maximum degree: 90 | |
| Time resolution | Monthly solutions | |
| Mission(s) | GRACE | GRACE-FO | |
| Instrument(s) / Captor(s) | Star Camera Assembly (SCA), Accelerometer (ACC), K-Band Ranging (KBR), GPS |
Auxiliary datasets
The CNES Level 2A geopotential solutions were calculated for the GRACE period using OMP de-aliasing models based on the ERA-Interim reanalysis and the TUGO ocean model. For the GRACE-FO period, the CNES solutions were calculated relative to the AOD1B RL06 de-aliasing models produced by the GFZ (Dobslaw et al., 2017).
The Level 2A GRACE/GRACE-FO solutions express geopotential anomalies relative to background models. These models include, in particular, atmospheric and oceanic de-aliasing, ocean tides, solid Earth and polar tides, as well as the mean field model. The set of background models used is described in Lemoine et al., 2026.
Consequently, the redistributions of atmospheric and oceanic mass estimated by the dealiasing models are not included in the geopotential anomalies provided in these solutions. In cases where these signals are of geophysical interest—for example, for the study of atmospheric and/or oceanic circulation—they must be restored by the user. This restoration simply involves adding the dealiasing models to the geopotential anomalies.
Users are therefore invited to download:
- the monthly atmospheric (GAA) and ocean (GAB) dealiasing products based on ERA-Interim and TUGO and produced by the OMP for the GRACE period,
- the monthly AOD1B RL06 atmospheric (GAA) and ocean (GAB) dealiasing products produced by the GFZ for the GRACE-FO period
and to handle these products in the same way as the geopotential solutions.
Citation
J.-M. Lemoine, S. Bourgogne, A. Boughanemi, J. Pfeffer, and E. Pellereau. Geopotential solution cholesky monthly, 2025i. URL: https://geodes.cnes.fr/projects/l2a_cnes_sagsa_ggm_cho_1month/.
Bibliography
- Chen et al., 2022; Ditmar, 2018; Dobslaw et al., 2017; Kusche et al., 2009; Landerer et al., 2020; Lemoine et al., 2026; Tapley et al., 2004, 2019
- Chen, J., Cazenave, A., Dahle, C., Llovel, W., Panet, I., Pfeffer, J., & Moreira, L. (2022). Applications and Challenges of GRACE and GRACE Follow-On Satellite Gravimetry. Surveys in Geophysics, 43(1), 305‑345. https://doi.org/10.1007/s10712-021-09685-x
- Ditmar, P. (2018). Conversion of time-varying Stokes coefficients into mass anomalies at the Earth’s surface considering the Earth’s oblateness. Journal of Geodesy, 92(12), 1401‑1412. https://doi.org/10.1007/s00190-018-1128-0
- Dobslaw, H., Bergmann-Wolf, I., Dill, R., Poropat, L., Thomas, M., Dahle, C., Esselborn, S., König, R., & Flechtner, F. (2017). A new high-resolution model of non-tidal atmosphere and ocean mass variability for de-aliasing of satellite gravity observations : AOD1B RL06. Geophysical Journal International, 211(1), 263‑269. https://doi.org/10.1093/gji/ggx302
- Kusche, J., Schmidt, R., Petrovic, S., & Rietbroek, R. (2009). Decorrelated GRACE time-variable gravity solutions by GFZ, and their validation using a hydrological model. Journal of Geodesy, 83(10), 903‑913. https://doi.org/10.1007/s00190-009-0308-3
- Landerer, F. W., Flechtner, F. M., Save, H., Webb, F. H., Bandikova, T., Bertiger, W. I., Bettadpur, S. V., Byun, S. H., Dahle, C., Dobslaw, H., Fahnestock, E., Harvey, N., Kang, Z., Kruizinga, G. L. H., Loomis, B. D., McCullough, C., Murböck, M., Nagel, P., Paik, M., … Yuan, D.-N. (2020). Extending the Global Mass Change Data Record : GRACE Follow-On Instrument and Science Data Performance. Geophysical Research Letters, 47(12), e2020GL088306. https://doi.org/https://doi.org/10.1029/2020GL088306
- Lemoine, J.-M., Bourgogne, S., Gégout, P., Reinquin, F., Marty, J.-C., Mercier, F., Loyer, S., Bruinsma, S., & Balmino, G. (2026). 22 years of time-variable gravity field determination from GRACE and GRACE Follow-On : The CNES/GRGS RL05 solution. Journal of Geodesy, 100(2), 20. https://doi.org/10.1007/s00190-026-02040-1
- Tapley, B. D., Bettadpur, S., Watkins, M., & Reigber, C. (2004). The gravity recovery and climate experiment : Mission overview and early results. Geophysical Research Letters, 31(9), n/a-n/a. https://doi.org/10.1029/2004gl019920
- Tapley, B. D., Watkins, M. M., Flechtner, F., Reigber, C., Bettadpur, S., Rodell, M., Sasgen, I., Famiglietti, J. S., Landerer, F. W., Chambers, D. P., Reager, J. T., Gardner, A. S., Save, H., Ivins, E. R., Swenson, S. C., Boening, C., Dahle, C., Wiese, D. N., Dobslaw, H., … Velicogna, I. (2019). Contributions of GRACE to understanding climate change. Nature Climate Change, 9(5), 358‑369. https://doi.org/10.1038/s41558-019-0456-2
