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| Payload weight | 65,000 lbs would be nice |
| Orbit | 115 nmi @ 28.5 deg orbital inclination |
| Payload Envelope Diameter | 180 inches |
| Payload Envelope Length | 780 inches |
| Cryogenics in payload | yes |
| Keep-alive power | supplied by payload after launch |
| Telemetry | not required before payload deployment |
| Deployment Mechanism | pyro bolts and springs |
| Flight 1 | +/- 30 nmi, +/- 2 deg inclination |
| Subsequent launch | +/- 2 nmi, +/- 0.2 deg inclination (Driven by rndz requirements) |
| Rotation | < 1 deg/sec, all axes |
| Relative Velocity | < 25 ft/sec, all axes |
| Rndz Responsibility | Payload |
| Prior to Payload Deploy | Launcher |
| After Payload Deploy | Payload |
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