| Prime manufacturer | Boeing Satellite Systems |
| Platform | BSS-702HP |
| Operator | Inmarsat |
| Mass at launch | 5900 kg; BOL: 3750 kg |
| Dry Mass | kg |
| Basic shape | box |
| Dimension (stowed) | H= 6.98 m, W= 3.59 m, L= 3.27m |
| Dimension (in orbit) | H= 6.98 m, W antennas= 8.08 m, L solar arrays= 33.80 m |
| >Equipment and Antennas |
| Antenna Ka | 89 user beams generated by 2 transmit and 4 receive apertures |
| Repeater Ka | Bent-pipe repeater, Ka-band: 60:48 TWTAs |
| T&C RF | Ka and C-band |
| High Capacity | Six steerable spot beams fed by 12 130W TWTAs |
| Solar array | 2 deployable solar arrays |
| Stabilization | |
| Propulsion: |
| Liquid apogee engine | 445 N |
| Stationkeeping Thrusters | Xenon ion propulsion |
| Control Thrusters | 4 x 22N (Axial), 4 x 10N (radial) |
| Power |
| Solar Panels | 13.8 kW, end of life |
| Construction | Two wings each with five panels of gallium arsenide solar cells |
| Batteries | Dual Li-Ion batteries |
| Design lifetime | 15 yrs |