| Designation | 22796 / 93058B |
| Launch date | 12 Sep 1993 |
| Country of origin | United States |
| Operator | NASA |
| Mission | Telecommunications |
| Geostationary orbit | see below |
| Launch vehicle | STS 51 |
| Begin | End | Position |
| L: 12 Sep 1993 | Jun 2000 | 100°W |
| Aug 2000 | 105°W, inclined |
| Prime contractor | GE Astro Space |
| Platform | GE-4000 modified |
| Mass at launch | 2545 kg |
| Mass in orbit | 1555 kg |
| Dimensions | 2.03 x 2.13 x 1.92 m |
| Stabilization | 3-axis |
| DC power |
BOL:
1770 W (batteries: 2 NiCd of 19 AH each) EOL: 1418 W (no payload operation during eclipse) |
| Design lifetime | 4 years |
| Telemetry & Command | Ka-band with backup in C-band |
| Main transponders | 4 |
| Backup transponders | |
| Power | 40 W (TWTA) |
| Bandwidth | 900 MHz |
| Coverage |
A
beam-forming network of 45 horns gives a coverage of about 20% of CONUS
providing 3 x 0.3° fixed beams There is a single 1.0° mechanically steered beam |
| EIRP max |
spot
beam: 60 dBW contiguous sectors: 59 dBW steerable: 53 dBW |
| Polarization | linear H/V |