STEP 1 |
USA |
| Designation | 94F03 |
| Launch date | 28 Jun 1994 |
| Launch site | Va, L-1011, RW30/12 |
| Launch vehicle | Pegasus-XL (#6) |
| Mission | Military: technology |
| Out of service | 27 Jun 1994 |
| Cause | Destroyed on launch with the launcher |
| Prime contractor | TRW |
| Platform | STEP |
| Mass at launch | |
| Mass in orbit | |
| Dimension | |
| Solar array | |
| Stabilization | 3-axis |
| DC power | 105 W |
| Design lifetime | 1 year |