NATO-3D |
NATO |
Spacecraft n°: |
NATO satellite n°: 6 |
| Designation | 15391 / 84115A |
| Launch date | 14 Nov 1984 - 00:34 UT |
| Launch site | CC, LC-17A |
| Launch vehicle | Delta-3914 (#D177) |
| Mission | Military: telecommunications |
| Geostationary orbit on: | |
| Perigee / Apogee | km |
| Eccentricity | |
| Inclination | ° |
| Period | min |
| Prime contractor | Ford Aerospace |
| Operator | |
| Platform | |
| Mass at launch | 720 kg? |
| Dry Mass | 385 kg ? |
| Basic shape | |
| Dimension (m) | 2.13 m (dia) x 2.74 m (high) |
| Solar array | |
| Stabilization | |
| DC power | 500 W |
| Design lifetime |
| Begin | End | Position |
| L: 14 Nov 1984 | ||
| Feb 1995 | Mar 1997 | 21°W, inclined |
| Apr 1997 | 18.5°W, inclined |