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WGS F4 (USA 233) (38070)
COSPAR: 2012-003A | Alt Name: WGS SV-4
Image
Additional Sources
Launch Details
Launch Date
January 20, 2012
Launch Site
Launch Pad
SLC37B
Launch Vehicle
Delta 4M+(5,4)
Orbital Elements
NORAD ID
38070
International Designator
2012-003A
Epoch
Thu, 02 Jul 2026 19:10:59 GMT
Apogee
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Perigee
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Inclination
0.02°
Right Ascension
33.44°
Eccentricity
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Argument of Perigee
91.95°
Period
1436.15 min
Mean Motion
1.00 rev/day
Latitude
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Longitude
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Altitude
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Velocity
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Polar Plot
3D Visualization
Basic Satellite Info
Name
WGS F4 (USA 233)
Alternative Name
WGS SV-4
Type
Payload
Status
Operational
Owner
AFSMC
Country
United States
Constellation
N/A
Related Satellites
Major Events
N/A
Latest TLEs
1 38070U 12003A 26183.79930490 .00000000 00000-0 00000-0 0 9995
2 38070 0.0212 33.4355 0001623 91.9508 171.6061 1.00267905 44305
Source: Celestrak
Summary
WGS F4 (USA 233), also known as WGS SV-4, is a communication satellite operated by AFSMC, launched on January 20, 2012, from Cape Canaveral Air Force Station using a Delta 4M+(5,4) launch vehicle. The spacecraft has dimensions of 6 meters in length and 3 meters in diameter with a span of 40.9 meters due to its solar arrays. It carries a cross-band payload including X-band, Global Broadcast, and 2-way Ka-band systems for communication purposes. With a dry mass of 2500 kg and a launch mass of 5768 kg, the satellite is equipped with deployable solar arrays and batteries for power generation. Manufactured by BOES using the BSS-702HP bus configuration, WGS F4 has an expected lifetime of 14 years and serves as part of the Wideband Global Satcom system for communication missions.
Physical Characteristics
Length
6
Diameter
3
Span
40.9
Dry Mass
2500
Launch Mass
5768
Shape
Box + 2 Pan
Radar Cross Section
15.8583
Visual Magnitude
Unknown
Color
Unknown
Material Composition
Unknown
Technical Details
Payload
Wideband Global Satcom 4
Purpose
Communication
Mission
Communication
Manufacturer
BOES
Life Expectancy
14 years
Bus
BSS-702HP
Configuration
BSS-702
Motor
R-4D-15-375
Equipment
Cross-band (X-band, Global Broadcast, 2-way Ka-band) payload
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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