Background Nanosatellites, otherwise known as nanosats, are given that name because of their size. The classification of all satellites distinguishes them into two general categories according to their weight. Large satellites weigh more than 1000 kilograms, while medium crafts weigh from 500 to 1000 kilograms. The mass of a small satellite does not exceed 500 kilograms, and this category also has many subgroups (Bandyopadhyay et al. 2016). A nanosatellite is one of the smallest devices of this type, being bigger only than pico and femto sats. One nanosat can weigh between one and ten kilograms. It usually resembles a little cube, although its shapes may vary depending on the sat’s purpose ( The National 2017). It is interesting that most pico and femto satellites require additional sources of manipulation, while the majority of launched nanosats can communicate with ground control on their own. Nanosatellites are currently gaining more and more popularity in industries that are interested in commercial and research opportunities because the benefits of their production process are hard to overlook. Description of Nanosatellites As nanosatellites gain commercial interest due to their cost efficiency, their outer appearance and inner structure become easy to describe. Most nanosatellites come in a cubic shape. The CubeSat, the most widespread version of a nanosat, is a cube with a mass of one kilogram and dimensions measuring ten centimeters per side (Oi et al. 2017). This satellite is fully functional, but it can be bundled in a group to form a constellation of sats with different functions. One block has two primary duties – a platform system, which acts similarly to a spacecraft, and a payload, which leaves space for other features. Platform systems are responsible for power generation, communication, and control. In stats’ constellations, some blocks can leave more room for payload, as one block cannot carry much weight or volume on its own. Nanosatellites are supported by electrical power generated with the help of solar panels. They usually use Lithium-Ion batteries which store the energy that can be used during an eclipse. Satellites go in and out of sunlight during their movement, so the cells are a necessary addition to the load. The placement of solar panels can differ from one model to another. As sats go on differing missions, some blocks may require more power than others. Placing solar panels only on the body of a nanosat may result in an insufficient amount of energy being produced. Oi et al. (2017) recommend building nanosatellites with solar panels on the sides of the cube, as well as installing some deploying solar arrays. The battery should have more storage than it can use during an eclipse because battery capacity decreases with time. All nanosatellites carry a computer on board, which functions as a sat’s operator. It receives commands and controls the electric power system. It also uses a radio to communicate with ground control. Benefits and Drawbacks of Nanosatellites Such devices are built small for many reasons. First, the production costs for nanosats are significantly lower than those of larger variations. The overall value of one satellite depends on its materials, production, and launch procedure. As nanosats are much smaller in size than other satellites, they are more economical in the use of materials during their manufacture. The process of building is also cheaper, although it has to be highly refined t