Spacecraft data:
| Prime manufactor | Orbital Sciences Corporation (OSC) |
| Platform | Star-2.4 bus |
| Operator | Intelsat, Ltd. |
| Mass at launch | 3200 kg |
| Dry Mass | 1440 kg |
| Basic shape | |
| Dimension (m) | 5.5 m x 3.3 m x 2.7 m |
| Equipment | 24 C-band transponders, 12 Ku-band transponders |
| Solar array | 2 deployable solar arrays |
| Stabilization | 3-axis |
| Propulsion | Monopropellant (hydrazine) system: IHI BT-4 |
| DC power | |
| Coverage | Asia Pacific Region |
| Design lifetime | 15 yrs - still active |
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