Program: Stacksat |
USA |
| Designation |
POGS or USA 56: 20560 / 90031A TEX or USA 57: 20561 / 90031B SCE or USA 58: 20562 / 90031C |
| Launch date | 11 Apr 1990 |
| Launch site | Va, SLC-3W |
| Launch vehicle | Atlas-E Altair-3A (#51) |
| Mission | Military: study ionospheric effects on signal propagation |
| Earth orbit: | |
| Perigee/Apogee | 741 km |
| Inclination | 90° |
| Period | |
| Prime contractor | CTA |
| Platform | |
| Mass at launch | 68 kg each |
| Mass in orbit | |
| Dimension | |
| Solar array | 15 W |
| Stabilization | gradient |
| DC power | |
| Design lifetime | 3 years |