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KANOPUS-V 4 (43181)
COSPAR: 2018-014B | Alt Name: Kanopus-V No. 4
Image
Additional Sources
Launch Details
Launch Date
February 1, 2018
Launch Site
VOSTO
Launch Pad
PU1S
Launch Vehicle
Soyuz-2-1A
Orbital Elements
NORAD ID
43181
International Designator
2018-014B
Epoch
Sat, 04 Jul 2026 07:48:31 GMT
Apogee
Calculating...
Perigee
Calculating...
Inclination
97.36°
Right Ascension
90.66°
Eccentricity
Calculating...
Argument of Perigee
92.11°
Period
94.55 min
Mean Motion
15.23 rev/day
Latitude
Calculating...
Longitude
Calculating...
Altitude
Calculating...
Velocity
Calculating...
Polar Plot
3D Visualization
Basic Satellite Info
Name
KANOPUS-V 4
Alternative Name
Kanopus-V No. 4
Type
Payload
Status
Operational
Owner
VNIIEMI
Country
Russia
Constellation
N/A
Related Satellites
Major Events
N/A
Latest TLEs
1 43181U 18014B 26185.32536564 .00003067 00000-0 13320-3 0 9995
2 43181 97.3572 90.6612 0001616 92.1108 268.0314 15.23053244467348
Source: Celestrak
Summary
KANOPUS-V 4, also known as Kanopus-V No. 4, is an Earth observation satellite based on the Kanopus bus configuration and was launched by VNIIEMI on February 1, 2018, from Vostochny Cosmodrome using a Soyuz-2-1A launch vehicle. The spacecraft has dimensions of 1 meter in length, 0.6 meters in diameter, and spans up to 6 meters with its solar arrays deployed. It carries PSS (Panchromatic Stereo Camera) and MSS (Multispectral Scanner) equipment for Earth observation purposes. KANOPUS-V 4 has a dry mass of 490 kg and uses two SPT-50 thrusters for maneuvering, powered by two deployable fixed solar arrays and batteries. The satellite is expected to have an operational lifetime of approximately five years.
Physical Characteristics
Length
1
Diameter
0.6
Span
6
Dry Mass
490
Launch Mass
490
Shape
Box+ 2 pan
Radar Cross Section
Unknown
Visual Magnitude
Unknown
Color
Unknown
Material Composition
Unknown
Technical Details
Payload
Kanopus-V
Purpose
Earth Observation
Mission
Earth Observation
Manufacturer
VNIIEMI
Life Expectancy
5 years
Bus
Kanopus
Configuration
Kanopus bus
Motor
2 x SPT-50
Equipment
PSS, MSS
Power System
2 deployable fixed 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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