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COSMOS 2376 [GLONASS] (26565)
COSPAR: 2000-063B | Alt Name: Kosmos-2375
Image
![COSMOS 2376 [GLONASS] Satellite Image](/images/sat/26565.jpg)
Additional Sources
Launch Details
Launch Date
October 13, 2000
Launch Site
Launch Pad
LC81/24
Launch Vehicle
Proton-K/DM-2
Orbital Elements
NORAD ID
26565
International Designator
2000-063B
Epoch
Tue, 30 Jun 2026 19:42:14 GMT
Apogee
Calculating...
Perigee
Calculating...
Inclination
65.20°
Right Ascension
313.39°
Eccentricity
Calculating...
Argument of Perigee
30.06°
Period
675.73 min
Mean Motion
2.13 rev/day
Latitude
Calculating...
Longitude
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Altitude
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Velocity
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Polar Plot
3D Visualization
Basic Satellite Info
Name
COSMOS 2376 [GLONASS]
Alternative Name
Kosmos-2375
Type
Payload
Status
Non-operational
Owner
VKSR/IACG
Country
Russia
Constellation
N/A
Related Satellites
Major Events
N/A
Latest TLEs
1 26565U 00063B 26181.82099780 -.00000058 00000-0 00000-0 0 9998
2 26565 65.1957 313.3929 0004826 30.0588 327.9613 2.13102573200101
Source: Celestrak
Summary
The COSMOS 2376 [GLONASS] satellite, also known as Kosmos-2375, is a navigation satellite launched on October 13, 2000, from the TYSMC launch site using LC81/24 and the Proton-K/DM-2 launch vehicle. It has a configuration of 3-Axis stabilized with dimensions of 4 meters in length, 1.5 meters in diameter, and a span of 7.8 meters. The satellite's dry mass is 1200 kg, and it was manufactured by POL for the VKSR/IACG. Its payload includes the Uragan No. 87L equipment, which supports its navigation mission. Power is provided by two deployable solar arrays and batteries. The satellite has a lifetime of approximately 3 years and its shape consists of a cylinder with antennas and two panels, with a radar cross-section (RCS) of 2.5118.
Physical Characteristics
Length
4
Diameter
1.5
Span
7.8
Dry Mass
1200
Launch Mass
1300
Shape
Cyl + Ant + 2 Pan
Radar Cross Section
2.5118
Visual Magnitude
Unknown
Color
Unknown
Material Composition
Unknown
Technical Details
Payload
Uragan No. 87L
Purpose
Navigation
Mission
Navigation
Manufacturer
POL
Life Expectancy
3 years
Bus
Uragan
Configuration
3-Axis stabilized
Motor
?
Equipment
?
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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