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GIOTTO (15875)
COSPAR: 1985-056A | Alt Name: Giotto
Image
Additional Sources
Launch Details
Launch Date
July 2, 1985
Launch Site
FRGUI
Launch Pad
ELA1
Launch Vehicle
Ariane 1
Orbital Elements
NORAD ID
15875
International Designator
1985-056A
Epoch
Wed, 03 Jul 1985 17:08:54 GMT
Apogee
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Perigee
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Inclination
6.99°
Right Ascension
264.81°
Eccentricity
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Argument of Perigee
178.00°
Period
631.54 min
Mean Motion
2.28 rev/day
Latitude
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Longitude
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Altitude
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Velocity
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Polar Plot
3D Visualization
Basic Satellite Info
Name
GIOTTO
Alternative Name
Giotto
Type
Payload
Status
Non-operational
Owner
ESA
Country
European Space Agency
Constellation
N/A
Related Satellites
Major Events
N/A
Latest TLEs
1 15875U 85056 A 85183.71452432 .00000000 +00000-0 +00000-0 0 9993
2 15875 006.9865 264.8091 7301153 177.9963 187.9371 02.28014901000029
Source: Celestrak
Summary
GIOTTO, also known as Giotto, is an ESA-owned satellite with the OBJECT_ID 1985-056A and NORAD_CAT_ID 15875. Launched on July 2, 1985, from ELA1 at FRGUI using an Ariane 1 launch vehicle, GIOTTO was designed for a comet flyby mission. The satellite is cylindrical in shape with dimensions of 2.9 meters in length and diameter, and weighs 476 kilograms dry and 545 kilograms at launch. It was manufactured by BAES and powered by solar cells and batteries. The spacecraft's primary purpose and mission were focused on the comet flyby, using Mage 1S motors for propulsion.
Physical Characteristics
Length
2.9
Diameter
1.9
Span
2.9
Dry Mass
476
Launch Mass
545
Shape
Cyl
Radar Cross Section
Unknown
Visual Magnitude
Unknown
Color
Unknown
Material Composition
Unknown
Technical Details
Payload
Giotto
Purpose
Comet flyby
Mission
Comet flyby
Manufacturer
BAES
Life Expectancy
Unknown
Bus
ESA Geos
Configuration
Unknown
Motor
Mage 1S
Equipment
Unknown
Power System
Solar cells, batteries
ADCS
Unknown
Transmitter Frequency
Unknown
Map
Next Pass
Azimuth Elevation Time (Local)
Start Azimuth
Max Elevation
Stop Azimuth
Time Until
Pass Duration
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