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MIR (16609)
COSPAR: 1986-017A | Alt Name: Mir
DECAYED
Image
Additional Sources
Launch Details
Launch Date
February 19, 1986
Launch Site
Launch Pad
LC1
Launch Vehicle
Soyuz-U
Orbital Elements
NORAD ID
16609
International Designator
1986-017A
Decay Date
3/23/2001
Basic Satellite Info
Name
MIR
Alternative Name
Mir
Type
Payload
Status
Decayed
Owner
NPOE
Country
USSR
Constellation
N/A
Related Satellites
Major Events
N/A
Summary
The MIR satellite, also known as Mir, is a space station core module manufactured by ZIKH for NPOE and launched on February 19, 1986, from the TYMSC site using LC1 launch pad with a Soyuz-U launch vehicle. It has dimensions of 13.1 meters in length, 4.2 meters in diameter, and a span of 13.1 meters. The satellite's dry mass is 20,100 kg, which is the same as its launch mass. MIR features two deployable solar arrays and batteries for power generation. Its design was intended for a five-year mission but achieved an operational lifetime of seventeen years. The satellite has a shape described as Step Cyl + 2 Pan, with an RCS value of 364.6535. It is part of the Almaz bus and DOS type configuration.
Physical Characteristics
Length
13.1
Diameter
4.2
Span
13.1
Dry Mass
20100
Launch Mass
20100
Shape
Step Cyl + 2 Pan
Radar Cross Section
364.6535
Visual Magnitude
Unknown
Color
Unknown
Material Composition
Unknown
Technical Details
Payload
DOS 7K No. 7
Purpose
Space station core module
Mission
Space station core module
Manufacturer
ZIKH
Life Expectancy
5 years (design); 17 years (achieved)
Bus
Almaz
Configuration
DOS type
Motor
Unknown
Equipment
Unknown
Power System
2 deployable solar arrays, batteries
ADCS
Unknown
Transmitter Frequency
Unknown
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