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| Spacecraft Mass | 125 kg |
| Electric Power System Mass | 14.7 kg |
| Command and Data Handling Mass | 11.5 kg |
| Communications Mass | 8.1 kg |
| Attitude Control System Mass | 8.3 kg |
| Thermal System Mass | 0.3 kg |
| Structures Mass and what it is made of | 7.8 kg |
| Lifetime (Months) | 12 |
| Battery Type | NiCad |
| Battery Capacity (A-hrs) | 4.8 |
| Begin of Life Power (watts) | 31 W |
| Solar Array Makeup | Fixed panel |
| Number of Kilobytes of Data Downloaded per Day | 20 MB ave 40 MB burst |
| Kilobytes per Second Downloaded | 32 |
| Number of Kilobytes Uploaded per Uplink | 4 |
| Bit Error Rate | Link dependent |
| Power Available for Communications (watts) | 1.8 Wave (22.4 Wave) |
| Whether it uses X-band or S-band Communication | S-Band |
| 3 Axis or Spin Stabilized | Spin Stabilized |
| Propulsion System? | None |
| Apogee (km) | 550 |
| Pointing Accuracy (degrees) | 0.25 |
| Pointing Knowledge (degrees) | 0.25 |