| | Glory | E1P | Hermes | KySat 1 |
| Prime manufactor | Orbital Sciences Corporation (OSC) | Montana Space Grant Consortium | Colorado Space Grant Consortium (CoSGC) | Kentucky Space |
| Platform | LEOStar | CubeSat | CubeSat | CubeSat |
| Operator | NASA | Montana Space Grant Consortium | Colorado Space Grant Consortium (CoSGC) | Kentucky Space |
| Mass at launch | 545 kg | 1 kg | 1 kg | 1 kg |
| Dry Mass | kg | | | |
| Basic shape | | | | |
| Dimension (m) | | | | |
| Equipment | | | | |
| Solar array | 2 deployable solar arrays | Solar cells | Solar cells | Solar cells |
| Stabilization | | | | |
| Propulsion | 45 kg, monopropellant blowdown, 4 × 4N thrusters | None | None | None |