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Today's brief covers significant advancements in space satellite launches, military spending impacts on space, and notable developments from the Space Force and SpaceX.
KONDOR-E (40353)
COSPAR: 2014-084A | Alt Name: Kondor-E
DECAYED
Image
Additional Sources
Launch Details
Launch Date
December 19, 2014
Launch Site
Launch Pad
LC175/59
Launch Vehicle
Strela
Orbital Elements
NORAD ID
40353
International Designator
2014-084A
Decay Date
10/22/2022
Basic Satellite Info
Name
KONDOR-E
Alternative Name
Kondor-E
Type
Payload
Status
Decayed
Owner
SANDF
Country
South Africa
Constellation
N/A
Related Satellites
Major Events
N/A
Summary
KONDOR-E is an Earth observation satellite using radar technology, launched on December 19, 2014, from TYMSC LC175/59, utilizing a Strela launch vehicle. This satellite, based on the Kondor-E bus design and manufactured by NPOMAO for SANDF (South African National Defence Force), has dimensions of 2.5 meters in length, 0.8 meters in diameter, and a span of 5 meters. It weighs 1150 kg at launch and is equipped with an S-band SAR payload. The satellite's power system consists of two deployable solar arrays and batteries. With a box shape including panels and dish antennas, KONDOR-E has been operational since its deployment and was designed for a five-year lifespan dedicated to Earth observation missions.
Physical Characteristics
Length
2.5
Diameter
0.8
Span
5
Dry Mass
1150
Launch Mass
1150
Shape
Box+2 pan+dish
Radar Cross Section
9.9039
Visual Magnitude
Unknown
Color
Unknown
Material Composition
Unknown
Technical Details
Payload
Kondor-E No. 0004
Purpose
Earth observation, radar
Mission
Earth observation, radar
Manufacturer
NPOMAO
Life Expectancy
5 years
Bus
Kondor
Configuration
Kondor-E bus
Motor
Unknown
Equipment
S-band SAR
Power System
2 deployable solar arrays, batteries
ADCS
Unknown
Transmitter Frequency
Unknown
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