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SPOT 3 (22823)
COSPAR: 1993-061A | Alt Name: SPOT 3
Image
Additional Sources
Launch Details
Launch Date
September 26, 1993
Launch Site
FRGUI
Launch Pad
ELA2
Launch Vehicle
Ariane 40
Orbital Elements
NORAD ID
22823
International Designator
1993-061A
Epoch
Sat, 04 Jul 2026 01:55:18 GMT
Apogee
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Perigee
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Inclination
98.86°
Right Ascension
249.12°
Eccentricity
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Argument of Perigee
190.55°
Period
101.40 min
Mean Motion
14.20 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
SPOT 3
Alternative Name
SPOT 3
Type
Payload
Status
Non-operational
Owner
CNES
Country
France
Constellation
N/A
Related Satellites
Major Events
N/A
Latest TLEs
1 22823U 93061A 26185.08007792 .00000116 00000-0 75302-4 0 9990
2 22823 98.8562 249.1231 0016522 190.5544 169.5288 14.20098041696978
Source: Celestrak
Summary
SPOT 3 is an Earth observation satellite, officially designated as 1993-061A, with a NORAD catalog ID of 22823. Launched on September 26, 1993, from the ELA2 pad at the Guiana Space Centre using an Ariane 40 launch vehicle, SPOT 3 was manufactured by MMST and owned by CNES (Centre National d'Études Spatiales). The satellite is configured as a SPOT Mk.1 with dimensions of 4.5 meters in length, 2 meters in diameter, and spans 8.2 meters when deployed. It has a dry mass of 1750 kg and a launch mass of 1900 kg. Equipped with two High Resolution Visible (HRV) imagers for Earth observation, SPOT 3 is powered by deployable solar arrays and batteries. The satellite's shape consists of a box section plus a pan configuration, with a radar cross-section of 6.3479 m². Its mission was designed to last for three years, focusing on Earth observation tasks through its onboard imaging systems.
Physical Characteristics
Length
4.5
Diameter
2
Span
8.2
Dry Mass
1750
Launch Mass
1900
Shape
Box + Pan
Radar Cross Section
6.3479
Visual Magnitude
Unknown
Color
Unknown
Material Composition
Unknown
Technical Details
Payload
SPOT 3
Purpose
Earth observation
Mission
Earth observation
Manufacturer
MMST
Life Expectancy
3 years (design)
Bus
SPOT
Configuration
SPOT Mk.1
Motor
SPOT AOCS
Equipment
2 HRV imager
Power System
Deployable solar array, 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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