experimental

Entrée : SPOT-1

URI: https://terra-vocabulary.org/ncl/FAIR-Incubator/earthscienceplatforms/c_17da39d1

The SPOT-1 (Satellite Pour l'Observation de la Terre) spacecraft was launched on February 22, 1986. SPOT-1 is an earth observation satellite with a greater ground resolution than that of the Landsat series satellites. The main applications for the images returned by the first 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: 101.40 m Inclination: 98.70 degrees Eccentricity: 0.00101 Periapsis: 815.00 km Apoapsis: 829.60 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-1 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. SPOT-1 consists of two identical high-resolution visible (HRV) imaging instruments and a package comprising two magnetic-tape data recorders and a telemetry transmitter.

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est un Concept | Platform
soumis parViqui Agazzi
accepté le 19 Sep 2022 08:12:55.742

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date accepted 19 Sep 2022 08:12:55.742
date submitted 19 Sep 2022 08:09:54.944
definition
entity SPOT-1
source graph graph

item class Platform | Concept
label SPOT-1
notation c_17da39d1
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-1 (Satellite Pour l'Observation de la Terre) spacecraft was launched on February 22, 1986. SPOT-1 is an earth observation satellite with a greater ground resolution than that of the Landsat series satellites. The main applications for the images returned by the first 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: 101.40 m Inclination: 98.70 degrees Eccentricity: 0.00101 Periapsis: 815.00 km Apoapsis: 829.60 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-1 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. SPOT-...
exact match 807f2f4d 1c2e 43ed 87f2 17d7dcced093
label SPOT-1
pref label SPOT-1
type Concept | Platform