[1] It's a minisatellite designed to accommodate new technology payloads in a quick turn-around time.

The structure includes a Starsensor (mSS), 4π Sunsensor (4πSS), micro-Inertial Reference Unit (mIRU), and a Magnetometer.

[3] It has 1N Thrusters (1Nms), 0.02Nm Reaction Wheels, and 20 A.m2 Magnetic Torquers powered by 5 kg of hydrazine fuel.

The altitude and orbital control system (AOCS) has a pointing accuracy of – 0.1° (3σ) and a drift rate of – 7.5e-4°/s.

During a massive Solar Storm in May 2024, EOS-07 had a higher than normal decay observed at 600meters, as compared to 300 for regular operations.