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Object Name | SAN MARCO 1 |
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Object Full Name | - |
Norad ID | 957 |
Cospar ID | 1964-084A |
Object Type | Satellite |
Object Status | Decayed |
Object Class | - |
End of Life | - |
San Marco 1 was an Italian flight test of the satellite to furnish data on air density and ionosphere characteristics. The launch vehicle was provided by NASA and was launched with an Italian launch crew.
Launch Date | 1964-12-15 |
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Decay Date | 1965-09-13 |
Launch Vehicle | - |
Launch Site | Wallops Island, Virginia, USA |
Launch Provider | - |
Launch Provider Country | - |
Launch Mass | - |
Dry Mass | - |
User | - |
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Mission | - |
Mission Detail | - |
Country of Registry | - |
Programme | - |
Operator | - |
Country of Operator | Italy |
Contractor | - |
Country of Contractor | - |
Payload Contractor | - |
Payload Contractor Country | - |
Orbit Status | Earth Orbit |
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Orbit | - |
Orbit Type | - |
Period: | 87.9 min |
Inclination: | 37.8° |
Apogee: | 185.0 km |
Perigee: | 151.0 km |
Longitude of Geo | - |
ECT | - |
Payload | - |
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Platform | - |
Propulsion | - |
Propulsion Type | - |
Life Time | - |
Power | - |
Budget | - |
Call Sign | - |
Beacon | - |
RCS | - |
References | - |
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Heights
Set
Pass Time
Visible
Time
Altitude
Azimuth
Time
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Azimuth
Time
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Angular Momentum: | - |
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Eccentricity: | - |
Inclination: | - |
RAAN: | - |
Argument of Perigee: | - |
True Anomaly: | - |
Period: | - |
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Semi-Major Axis: | - |
Perigee: | - |
Apogee: | - |
Mean Motion: | - |
Mean Anomaly: | - |
Latitude: | - |
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Longitude: | - |
Altitude: | - |
Speed: | - |
Azimuth: | - |
Elevation: | - |
Range: | - |