Intelsat-5 4 |
INTELSAT / US |
Spacecraft n°: |
INTELSAT spacecraft n°: 31 |
| Designation: | 13083 / 82017A |
| Launch date | 05 Mar 1982 |
| Launch site | CC, LC-36A |
| Launch vehicle: | Atlas-SLV3D Centaur-D1AR (AC-58) |
| Mission: | Telecommunications |
| Geostationary orbit on: | |
| Perigee / Apogee | km |
| Eccentricity | |
| Inclination | deg |
| Period | min |
| Prime manufacturer | Ford Aerospace |
| Platform | |
| Operator | Intelsat |
| Mass at launch | kg |
| Dry Mass | kg |
| Basic shape | |
| Dimension (m) | |
| Solar array | |
| Stabilization | |
| Propulsion | |
| DC power |
| Begin | End | Position |
| L: 5 Mar 1982 | ||
| Apr 1989 | went inclined | |
| Jan 1991 | Oct 1992 | 34.5°W, inclined |
| July 1993 | Sep 1993 | 32°W, inclined |
| Dec 1993 | Jan 1994 | 40.5°W, inclined |
| May 1994 | May 1995 | 31.5°W, inclined |
| Jul 1995 | Nov 1995 | 29.4°W, inclined |
| Out of service | late Nov 1995 |
| Cause | end of life: deorbited |