| Official name | ATLAS CENTAUR 2 R/B |
| Alternative name | CENTAUR C (Atlas LV3C) |
| Cospar ID | 1963-047A |
| Norad ID | 694 |
| Launch date | 1963-11-27 |
| Launch site | AFETR |
| Launch vehicle | Atlas-LV3C Centaur-B |
| Country/Organization | USA |
| Type application | Instrumented second stage |
| RCS size | LARGE |
| Decay date | ON ORBIT |
| Period (min) | 102.32 |
| Inclination (deg) | 30.36 |
| Perigee (km) | 458 |
| Apogee (km) | 1279 |
| Eccentricity | 0.47265400115141 |
| Mean motion (revs. per day) | 14.0734949179046 |
| Semi-Major axis (km) | 7246.635 |
| Raan (deg) | 321.1329 |
| Arg of perigee (deg) | 325.2517 |
| Shape | Cyl + 2 Nozzle |
| Mass (kg) | 4443 |
| Diameter (m) | 3.1 |
| Height (m) | 8.59 |
| Span (m^2) | 8.59 |
| Contractors | General Dynamics |
| Configuration | Instrumented Centaur |
| Power | Batteries |
| Satellite | COSPAR | Date | LS | Launch Vehicle | Remarks | |
|---|---|---|---|---|---|---|
| ATLAS CENTAUR 2 R/B | 1963-047A | 1963-11-27 | AFETR | Atlas-LV3C Centaur-B |
.png)
