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San Marco satellite

Spacecraft · Italy

Original archive entry. The text, images and links below are kept as they were written.

San Marco D/L
San Marco D/L
Credit: Manufacturer Image

Italian earth atmosphere satellite. Atmospheric density studies.

Country
Italy
Agency
CRS
Bibliography
2, 279, 6

Chronology

5 events

1964 December 15

20:20 GMT - . Launch Site: Wallops Island. Launch Complex: Wallops Island LA3A. LV Family: Scout. Launch Vehicle: Scout X-4.
  • San Marco 1 - . Mass: 254 kg (559 lb). Nation: Italy. Agency: CRS. Class: Earth. Type: Atmosphere satellite. Spacecraft: San Marco satellite. Decay Date: 1965-09-11 . USAF Sat Cat: 957 . COSPAR: 1964-084A. Apogee: 842 km (523 mi). Perigee: 200 km (120 mi). Inclination: 37.80 deg. Period: 95.10 min. Atmospheric density studies. Spacecraft engaged in research and exploration of the upper atmosphere or outer space (US Cat B). .

1967 April 26

10:06 GMT - . Launch Site: San Marco. LV Family: Scout. Launch Vehicle: Scout B.
  • San Marco 2 - . Payload: San Marco B. Mass: 129 kg (284 lb). Nation: Italy. Agency: CRS. Class: Earth. Type: Atmosphere satellite. Spacecraft: San Marco satellite. Decay Date: 1967-10-14 . USAF Sat Cat: 2761 . COSPAR: 1967-038A. Apogee: 741 km (460 mi). Perigee: 219 km (136 mi). Inclination: 2.90 deg. Period: 94.20 min. Atmospheric density data. Scientific satellite launched from a mobile range off Formosa Bay (Kenya). .

1971 April 24

07:32 GMT - . Launch Site: San Marco. LV Family: Scout. Launch Vehicle: Scout B.
  • San Marco 3 - . Payload: San Marco C. Mass: 164 kg (361 lb). Nation: Italy. Agency: CRS. Class: Earth. Type: Atmosphere satellite. Spacecraft: San Marco satellite. Decay Date: 1971-11-29 . USAF Sat Cat: 5176 . COSPAR: 1971-036A. Apogee: 707 km (439 mi). Perigee: 222 km (137 mi). Inclination: 3.20 deg. Period: 93.80 min. Atmospheric research. Spacecraft engaged in research and exploration of the upper atmosphere or outer space (US Cat B). .

1974 February 18

10:05 GMT - . Launch Site: San Marco. LV Family: Scout. Launch Vehicle: Scout D-1.
  • San Marco 4 - . Payload: San Marco C2. Mass: 164 kg (361 lb). Nation: Italy. Agency: CRS. Class: Earth. Type: Atmosphere satellite. Spacecraft: San Marco satellite. Decay Date: 1976-05-04 . USAF Sat Cat: 7154 . COSPAR: 1974-009A. Apogee: 875 km (543 mi). Perigee: 270 km (160 mi). Inclination: 2.90 deg. Period: 96.10 min. Measurement of density, temperature, composition of atmosphere. Launch time 10:05:28.5 GMT. Anticipated life: 3 years. .

1988 March 25

19:50 GMT - . Launch Site: San Marco. LV Family: Scout. Launch Vehicle: Scout G-1.
  • San Marco D/L - . Payload: San Marco 5. Mass: 236 kg (520 lb). Nation: Italy. Agency: ASI. Class: Earth. Type: Atmosphere satellite. Spacecraft: San Marco satellite. Decay Date: 1988-12-06 . USAF Sat Cat: 19013 . COSPAR: 1988-026A. Apogee: 625 km (388 mi). Perigee: 268 km (166 mi). Inclination: 3.00 deg. Period: 93.50 min. Upper atmosphere studies; US, France, Italy participation. .