Entrée : SPOT-3
URI: https://terra-vocabulary.org/ncl/FAIR-Incubator/earthscienceplatforms/c_bff14954
The SPOT-3 (Satellite Pour l'Observation de la Terre) spacecraft was launched in September 26,1993. SPOT-3 is a earth observation satellite with a ground resolution better than that of the Landsat series satellites. The main applications for the images returned by the third SPOT mission are land-use studies, agriculture and forestry resources, mineral and oil resources, and cartography. The three-axis stabilized satellite operates in a circular sun-synchronous near-polar orbit for a design lifetime of 2 years. Orbital Characteristics- Orbital Period: 101.20 m Inclination: 98.60 degrees Periapsis: 819.00 km Apoapsis: 846.00 km The spacecraft dimensions are 2 x 2 x 3.5 m and 15.60 m for the overall length of the deployed solar panel. SPOT-3 consists of two parts: (1) the bus, a standard multipurpose platform, and (2) the payload. The bus provides housekeeping information and an onboard computer. The payload is mounted on one of the side panels of the bus. It consists of two identical high-resolution visible (HRV) imaging instruments and a package comprising two magnetic-tape data recorders and a telemetry transmitter.
Métadonnées principales
est un | Concept | Platform |
soumis par | Viqui Agazzi |
accepté le | 19 Sep 2022 08:12:55.846 |
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date accepted |
19 Sep 2022 08:12:55.846
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date submitted |
19 Sep 2022 08:09:54.729
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definition |
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Platform
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SPOT-3
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notation |
c_bff14954
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register |
earthscienceplatforms
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status |
status experimental
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register item
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version info |
2
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Définition
broader |
SPOT
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definition |
The SPOT-3 (Satellite Pour l'Observation de la Terre) spacecraft was launched in September 26,1993. SPOT-3 is a earth observation satellite with a ground resolution better than that of the Landsat series satellites. The main applications for the images returned by the third SPOT mission are land-use studies, agriculture and forestry resources, mineral and oil resources, and cartography. The three-axis stabilized satellite operates in a circular sun-synchronous near-polar orbit for a design lifetime of 2 years. Orbital Characteristics- Orbital Period: 101.20 m Inclination: 98.60 degrees Periapsis: 819.00 km Apoapsis: 846.00 km The spacecraft dimensions are 2 x 2 x 3.5 m and 15.60 m for the overall length of the deployed solar panel. SPOT-3 consists of two parts: (1) the bus, a standard multipurpose platform, and (2) the payload. The bus provides housekeeping information and an onboard computer. The payload is mounted on one of the side panels of the bus. It consists of two identical ...
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exact match |
d333cd96 f1f0 4179 9fbc 162b18fcb8c8
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label |
SPOT-3
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pref label |
SPOT-3
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type |
Concept
| Platform
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