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This invention discloses a microsatellite configuration and assembly method suitable for mass production, belonging to the field of spacecraft technology. The microsatellite configuration includes: a satellite body; a satellite base plate module mounted on the bottom of the satellite body; a satellite electronics module mounted and connected to the rear of the satellite body; satellite Y-plates mounted on both sides of the satellite body, with the Y-plates fixedly connected to the sides of the satellite electronics module; a satellite X-plate mounted and connected to the front of the satellite body; and solar panels connected to both sides of the Y-plates. This invention adopts a modular design, dividing the satellite into two parts: an electronics module and a base plate module. This allows for parallel satellite assembly, reducing overall operation time, improving satellite maintainability, and simplifying operation.