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| Object Name | SPUTNIK 5 |
|---|---|
| Object Full Name | - |
| Norad ID | 55 |
| Cospar ID | 1960-011A |
| Object Type | Satellite |
| Object Status | Decayed |
| Object Class | - |
| End of Life | - |
This spacecraft was the second in a series of spacecraft designed to further the development of an Earth orbiting system for the planned manned space program. The spacecraft carried two dogs, Strelka (pictured) and Belka, in addition to a television system and other scientific instrumentation. After a one day flight, the spacecraft and both dogs were successfully recovered.
| Launch Date | 1960-08-19 |
|---|---|
| Decay Date | 1960-08-20 |
| Launch Vehicle | - |
| Launch Site | Baikonur Cosmodrome, Kazakhstan |
| Launch Provider | - |
| Launch Provider Country | - |
| Launch Mass | - |
| Dry Mass | - |
| User | - |
|---|---|
| Mission | - |
| Mission Detail | - |
| Country of Registry | - |
| Programme | - |
| Operator | - |
| Country of Operator | USSR/Russia |
| Contractor | - |
| Country of Contractor | - |
| Payload Contractor | - |
| Payload Contractor Country | - |
| Orbit Status | Earth Orbit |
|---|---|
| Orbit | - |
| Orbit Type | - |
| Period: | 90.7 min |
| Inclination: | 64.9° |
| Apogee: | 307.0 km |
| Perigee: | 307.0 km |
| Longitude of Geo | - |
| ECT | - |
| Payload | - |
|---|---|
| Platform | - |
| Propulsion | - |
| Propulsion Type | - |
| Life Time | - |
| Power | - |
| Budget | - |
| Call Sign | - |
| Beacon | - |
| RCS | - |
| References | - |
|---|
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| Angular Momentum: | - |
|---|---|
| Eccentricity: | - |
| Inclination: | - |
| RAAN: | - |
| Argument of Perigee: | - |
| True Anomaly: | - |
| Period: | - |
|---|---|
| Semi-Major Axis: | - |
| Perigee: | - |
| Apogee: | - |
| Mean Motion: | - |
| Mean Anomaly: | - |
| Latitude: | - |
|---|---|
| Longitude: | - |
| Altitude: | - |
| Speed: | - |
| Azimuth: | - |
| Elevation: | - |
| Range: | - |