EGU24-4232, updated on 08 Mar 2024
https://doi.org/10.5194/egusphere-egu24-4232
EGU General Assembly 2024
© Author(s) 2024. This work is distributed under
the Creative Commons Attribution 4.0 License.

Early evaluation of effects on Dual-frequency Precipitation Radar observations by the orbit boost of the GPM Core Observatory 

Takuji Kubota1, Takeshi Masaki2, Gennosuke Kikuchi2, Masato Ito2, Tomohiko Higashiuwatoko2, Kaya Kanemaru3, Nobuhiro Takahashi4, Kosuke Yamamoto1, Kinji Furukawa5, and Tomomi Nio6
Takuji Kubota et al.
  • 1Earth Observation Research Center, Japan Aerospace Exploration Agency, Tsukuba, Japan (kubota.takuji@jaxa.jp)
  • 2Remote Sensing Technology Center of Japan, Ibaraki, Japan
  • 3Radio Research Institute, National Institute of Information and Communications Technology, Tokyo, Japan
  • 4Institute for Space and Earth Environmental Research, Nagoya University, Nagoya, Japan
  • 5PMM Project team, Japan Aerospace Exploration Agency, Tsukuba, Japan
  • 6Satellite Applications and Operations Center, Japan Aerospace Exploration Agency, Tsukuba, Japan

The NASA and the JAXA performed orbit boost maneuvers in November 2023 that raised an altitude of the Global Precipitation Measurement (GPM) Core Observatory from 400 km to 435 km to extend its lifetime. Effects of the orbit boost on the spaceborne precipitation radar have been investigated in the Tropical Rainfall Measuring Mission (TRMM) performed in August 2001. This study evaluates effects on DPR observations due to the GPM orbit boost.

Firstly, spacecraft altitudes of the GPM Core Observatory were analyzed during the period from 13rd October to 17th November 2023. The minimum altitudes were changed from about 400 km to about 435 km by the orbit boost. The averaged altitudes were changed from about 407 km to about 442 km by it. Thus, 407km and 442km were adopted as typical averaged satellite altitudes in pre-boost and the post-boost, respectively.

Spatial resolution at the nadir and swath width is changed at 5.04km×5.04km and 255.8 km at satellite altitude of 407 km to 5.48km×5.48km and 277.9 km at satellite altitude of 442 km, respectively.  Distances between adjacent footprints in the cross-track direction between the pre-boost and the post-boost using observation data and they confirmed that changes of the sampling were larger in the cross-track direction (about 5 km to 5.5 km at the nadir).

It was found that the DPR coverage tendency was changed by the GPM orbit boost. In pre-boost, DPR achieved 100% coverage in 8 days. On the other hand, with post-boost, the coverage was still 99.9834% after 24 days, slightly less than 100%. This coverage trend is expected to change with satellite maneuvers. The maneuver is expected to change the orbit elements, thereby covering all locations.

The sensitivity degradation of the DPR is expected owing to the increase of satellite altitude. Measured radar reflectivity factor (Zm) at storm top height (STH) over the ocean for is used as an indicator of the sensitivity. With analyzing Zm at STH over the ocean, the sensitivity degradation was found for about 0.8-0.9dB for KuPR, and about 0.7-0.9dB for KaPR.

How to cite: Kubota, T., Masaki, T., Kikuchi, G., Ito, M., Higashiuwatoko, T., Kanemaru, K., Takahashi, N., Yamamoto, K., Furukawa, K., and Nio, T.: Early evaluation of effects on Dual-frequency Precipitation Radar observations by the orbit boost of the GPM Core Observatory , EGU General Assembly 2024, Vienna, Austria, 14–19 Apr 2024, EGU24-4232, https://doi.org/10.5194/egusphere-egu24-4232, 2024.