| Name of Satellite, Alternate Names | Iridium 14A (Iridium SV092) |
| Country of Operator/Owner | USA |
| Operator/Owner | Iridium Satellite LLC |
| Users | Government/Commercial |
| Purpose | Communications |
| Class of Orbit | LEO |
| Type of Orbit | Polar |
| Longitude of GEO (degrees) | 0 |
| Perigee (km) | 708 |
| Apogee (km) | 711 |
| Eccentricity | 0.000211879370012006 |
| Inclination (degrees) | 86.5 |
| Period (minutes) | 99 |
| Launch Mass (kg.) | 689 |
| Dry Mass (kg.) | 556 |
| Power (watts) | 1,400 (EOL) |
| Date of Launch | 11-06-1999 |
| Expected Lifetime | 8 yrs. |
| Contractor | Motorola Satellite Communications Group |
| Country of Contractor | USA |
| Launch Site | Taiyuan Launch Center |
| Launch Vehicle | Long March 2C |
| COSPAR Number | 1999-032A |
| NORAD Number | 25777 |
| Comments |