Thelma |
USA |
| Designation | 26093 / 00004L |
| Launch date | 27 Jan 2000 - 03:03 UT |
| Launch site | Va, SLC-8 |
| Launch vehicle | Minotaur (#1) |
| Mission | Technology |
| Earth orbit on Feb 15.22: | |
| Perigee / Apogee | 749 x 805 km |
| Eccentricity | 0.004 |
| Inclination | 100.22 deg |
| Period | 100.40 min |
| Prime contractor | - |
| Platform | OPAL satellite |
| Mass at launch | 0.50 kg |
| Mass in orbit | |
| Dimension | - |
| Solar array | none |
| Stabilization | none |
| DC power | |
| Design lifetime | 0.1 - 0.2 m |