experimental

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 parViqui Agazzi
accepté le 19 Sep 2022 08:12:55.846

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date accepted 19 Sep 2022 08:12:55.846
date submitted 19 Sep 2022 08:09:54.729
definition
entity SPOT-3
source graph graph

item class Platform | Concept
label SPOT-3
notation c_bff14954
register earthscienceplatforms
status status experimental
submitter
account name victoria.agazzi@teledetection.fr
name Viqui Agazzi

type register item
version info 2
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Définition

broader SPOT
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 ...
exact match d333cd96 f1f0 4179 9fbc 162b18fcb8c8
label SPOT-3
pref label SPOT-3
type Concept | Platform