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COSMOS 2403 [GLONASS] (28114)
COSPAR: 2003-056C | Alt Name: Kosmos-2404
Image
![COSMOS 2403 [GLONASS] Satellite Image](/images/sat/28114.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
28114
International Designator
2003-056C
Epoch
Sun, 28 Jun 2026 21:05:17 GMT
Apogee
Calculating...
Perigee
Calculating...
Inclination
64.28°
Right Ascension
61.83°
Eccentricity
Calculating...
Argument of Perigee
63.12°
Period
675.72 min
Mean Motion
2.13 rev/day
Latitude
Calculating...
Longitude
Calculating...
Altitude
Calculating...
Velocity
Calculating...
Polar Plot
3D Visualization
Basic Satellite Info
Name
COSMOS 2403 [GLONASS]
Alternative Name
Kosmos-2404
Type
Payload
Status
Non-operational
Owner
KVR/IACG
Country
Russia
Constellation
N/A
Related Satellites
Major Events
N/A
Latest TLEs
1 28114U 03056C 26179.87866976 -.00000038 00000-0 00000-0 0 9994
2 28114 64.2820 61.8347 0061608 63.1168 118.7997 2.13104707175498
Source: Celestrak
Summary
The COSMOS 2403 [GLONASS] satellite, also known as Kosmos-2404, was launched on December 10, 2003, from the Tsemel'nik Site (TYMSC) using a Proton-K/Briz-M launch vehicle. This navigation satellite is part of the Uragan series and uses a 3-Axis stabilized Uragan-M bus configuration. The spacecraft has dimensions of 4 meters in length, 1.5 meters in diameter, and a span of 7.8 meters when its solar arrays are deployed. It has a launch mass of 1415 kg and a dry mass of 1200 kg. Its power system includes two deployable solar arrays and batteries. The satellite's shape is described as cylindrical with antennas and panels, and it was manufactured by NPOPMR for the KVR/IACG. It has an expected lifetime of seven years and serves navigation purposes within its mission framework.
Physical Characteristics
Length
4
Diameter
1.5
Span
7.8
Dry Mass
1200
Launch Mass
1415
Shape
Cyl + Ant + 2 Pan
Radar Cross Section
5.0118
Visual Magnitude
Unknown
Color
Unknown
Material Composition
Unknown
Technical Details
Payload
Uragan-M No. 11L
Purpose
Navigation
Mission
Navigation
Manufacturer
NPOPMR
Life Expectancy
7 years
Bus
Uragan
Configuration
3-Axis stabilized Uragan-M bus
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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