| Prime contractor | Lockheed Martin (formerly GE Astro Space) |
| Platform | GE-4000 |
| Mass at launch | 1850-2000 kg |
| Dry mass | 895 kg |
| Mass in orbit | 1150 kg |
| Payload mass | 208 kg |
| Dimension | 2.1 x 1.8 x 1.7 m |
| Solar array | 16.7 m |
| Stabilization | 3-axis |
| DC power | 2800 W |
| Payload power | sunlight: 2138 W, eclipse: 1725 W |
| Design lifetime | 13 years |