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RADUGA 6 (11708)
COSPAR: 1980-016A | Alt Name: Raduga
Image
Additional Sources
Launch Details
Launch Date
February 20, 1980
Launch Site
Launch Pad
LC200/39
Launch Vehicle
Proton-K/DM
Orbital Elements
NORAD ID
11708
International Designator
1980-016A
Epoch
Fri, 03 Jul 2026 22:43:10 GMT
Apogee
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Perigee
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Inclination
5.67°
Right Ascension
286.46°
Eccentricity
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Argument of Perigee
323.62°
Period
1436.70 min
Mean Motion
1.00 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
RADUGA 6
Alternative Name
Raduga
Type
Payload
Status
Non-operational
Owner
GUKOSR
Country
USSR
Constellation
N/A
Related Satellites
Major Events
N/A
Latest TLEs
1 11708U 80016A 26184.94665436 .00000138 00000-0 00000-0 0 9998
2 11708 5.6745 286.4622 0002187 323.6202 61.0491 1.00230023122335
Source: Celestrak
Summary
RADUGA 6, also known as Raduga, is a communication satellite launched on February 20, 1980, from LC200/39 at TYMSC using the Proton-K/DM launch vehicle. It has a bus configuration of Raduga and carries a KAUR-3 payload. The spacecraft measures 5.5 meters in length, with a diameter of 2.5 meters and a span of 9.5 meters. At launch, it had a mass of 1965 kg and a dry mass of 1800 kg. It is equipped with 3 Delta-1 C-Band transponders and 3 Delta-2 C-Band transponders for communication purposes. The satellite's power supply consists of two deployable solar arrays and batteries. RADUGA 6 was manufactured by NPOPM and operated for approximately three years, serving the GUKOSR as part of its communication mission. Its shape is described as a step cylinder with two panels, and it has an RCS value of 1.2589.
Physical Characteristics
Length
5.5
Diameter
2.5
Span
9.5
Dry Mass
1800
Launch Mass
1965
Shape
Step Cyl + 2 Pan
Radar Cross Section
1.2589
Visual Magnitude
Unknown
Color
Unknown
Material Composition
Unknown
Technical Details
Payload
Gran' No. 16L
Purpose
Communication
Mission
Communication
Manufacturer
NPOPM
Life Expectancy
3 years
Bus
Raduga
Configuration
KAUR-3
Motor
Unknown
Equipment
3 Delta-1 C-Band transponders, 3 Delta-2 C-Band transponders
Power System
2 deployable solar arrays, 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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