Sistem monitoring penggunaan listrik baik secara prabayar maupun pascabayar masih memiliki beberapa masalah, salah satu permasalahan yang terjadi adalah masih kurangnya pengawasan untuk mengetahui seberapa besar penggunaan listrik di suatu rumah atau suatu daerah. Untuk mengatasi permasalahan tersebut, diperlukan sebuah perangkat yang mampu mengukur parameter-parameter pada listrik arus AC (Alternating Current) satu fasa, dan menampilkannya hasilnya dalam suatu sistem informasi, sehingga penggunaan daya listrik dari setiap rumah atau daerah dapat diketahui jumlahnya.Dengan menggunakan papan mikrokontroler Arduino Uno sebagai pengolah datanya, parameter yang dapat diukur oleh perangkat terdiri dari arus, tegangan dan daya, data pengukuran tersebut kemudian dikirim melalui jaringan wireless ke sebuah komputer server, komputer server berfungsi sebagai penyimpanan data hasil monitoring dan mengolah data tersebut menjadi sebuah informasi yang ditampilkan dalam sebuah website.Berdasarkan hasil pengujian pada pengukuran arus didapatkan nilai kesalahan rata-rata sebesar 3,28%, kesalahan rata-rata pengukuran tegangan sebesar 0,39%, pada pengukuran nilai daya didapatkan nilai kesalahan rata-rata sebesar 8,82%. Sedangkan pada proses pengiriman data diperoleh nilai presentase error sebesar 0.1%, dan akurasi data mencapai 100%.

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Locana Bhumi payload is one of the selected payloads in The 2nd GRSS Student Grand Challenge, and it will be installed in a 3U Cube Satellite. Its main mission is to monitor cloud coverage in several regions such as Indonesia, United Arab Emirates, Oman, and Australia. Clouds have a role in climate change, they are able to reflect infrared light and cool the surface of the earth that is covered by clouds. At the same time, clouds are also able to trap heat, as a result, they warm the earth. By monitoring cloud coverage over the selected areas, it is expected that we will be able to study how cloud coverage could affect the climate system on the earth. In order to monitor the cloud coverage, the Locana payload will capture cloud images by using a small serial camera that is equipped with a low voltage ¼-inch 5-megapixel OV5642 image sensor. This camera also employs a 4.14 mm focal length fixed-infrared-cut-filter lens. This camera is able to capture 500 x 375 km2 of the area from about 575 km above the earth's surface, with that area observation, the cloud coverage is expected to be easier to observe. In terms of image storage, this payload is integrated with a 1 Gigabit memory. This memory is also used for saving the payload housekeeping data. To prevent the payload from overcurrent situations, the payload system is integrated with an Over Current Protection module. Moreover, an alloy-based enclosure has been designed to protect the component from outer space radiation. The material used for the enclosure is aluminum alloy 7075. The payload has a compact dimension, which fits in 0.5U of Cube Satellite size. Currently, the development of this payload has reached the Critical Design Review stage and it is expected to be ready in Quartal-1 2022.