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COSMOS 2402 [GLONASS] (28113)
COSPAR: 2003-056B | Alt Name: Kosmos-2403
Image
![COSMOS 2402 [GLONASS] Satellite Image](/images/sat/28113.jpg)
Additional Sources
Launch Details
Launch Date
December 10, 2003
Launch Site
Launch Pad
LC81/24
Launch Vehicle
Proton-K/Briz-M
Orbital Elements
NORAD ID
28113
International Designator
2003-056B
Epoch
Mon, 29 Jun 2026 05:42:44 GMT
Apogee
Calculating...
Perigee
Calculating...
Inclination
64.28°
Right Ascension
61.77°
Eccentricity
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Argument of Perigee
72.42°
Period
675.72 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 2402 [GLONASS]
Alternative Name
Kosmos-2403
Type
Payload
Status
Non-operational
Owner
KVR/IACG
Country
Russia
Constellation
N/A
Related Satellites
Major Events
N/A
Latest TLEs
1 28113U 03056B 26180.23801118 -.00000035 00000-0 00000-0 0 9999
2 28113 64.2786 61.7689 0051395 72.4194 117.1525 2.13105098175506
Source: Celestrak
Summary
COSMOS 2402 [GLONASS], also known as Kosmos-2403, is a navigation satellite launched on December 10, 2003, from the TYMSC launch site using LC81/24 and Proton-K/Briz-M as its launch vehicle. The satellite has a bus configuration of Uragan and is 3-Axis stabilized. It measures 4 meters in length with a diameter of 1.5 meters and spans 7.8 meters when fully deployed, including solar arrays. Its dry mass is 1200 kg, and it had an initial launch mass of 1415 kg. The satellite was manufactured by POL (KVR/IACG) for navigation purposes and carries the Uragan No. 95L payload. It uses two deployable solar arrays and batteries for power supply and has a design lifetime of three years. Its shape is described as Cyl + Ant + 2 Pan, with an RCS value of 3.981.
Physical Characteristics
Length
4
Diameter
1.5
Span
7.8
Dry Mass
1200
Launch Mass
1415
Shape
Cyl + Ant + 2 Pan
Radar Cross Section
3.981
Visual Magnitude
Unknown
Color
Unknown
Material Composition
Unknown
Technical Details
Payload
Uragan No. 95L
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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