Falconsat |
USA |
Spacecraft n°: |
USA satellite n°: |
| Designation | 26064 / 00004D |
| Launch date | 27 Jan 2000 - 03:03 UT |
| Launch site | Va, SLC-8 |
| Launch vehicle | Minotaur (#1) |
| Mission | Technology |
| Earth orbit on Jan 27, 2000: | |
| Perigee / Apogee | 751 x 803 km |
| Eccentricity | 0.004 |
| Inclination | 100.38 deg |
| Period | 100.24 min |
| Manufacturer | USAFA (the US Air Force Academy) |
| Platform | Falconsat |
| Operator | USAF Academy |
| Mass at launch | 52 kg |
| Dry Mass | |
| Dimension | |
| Solar array | |
| Stabilization | |
| DC power | |
| Design lifetime |