JAWSAT |
USA |
| Designation | 26061 / 00004A |
| Launch date | 27 Jan 2000 - 03:03 UT |
| Launch site | Va, SLC-8 |
| Launch vehicle | Minotaur 10SP/SLV-1 (#1) |
| Mission | Technology |
| Earth orbit on 2000 Jan 27.31: | |
| Perigee / Apogee | 749 x 808 km |
| Eccentricity | 0.004 |
| Inclination | 100.23° |
| Period | 100.42 min |
| Manufacturer | Weber State |
| Bus | MPA |
| Operator | USAF AF Academy/Weber State |
| Mass at launch | 191.4 kg |
| Mass in orbit | 64 kg (satellite released) |
| Dimension | |
| Solar array | |
| Stabilization | |
| DC power | 80 W |
| Design lifetime |