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AMC-16 (28472)
COSPAR: 2004-048A | Alt Name: AMC 16
Image
Additional Sources
Launch Details
Launch Date
December 17, 2004
Launch Site
Launch Pad
SLC41
Launch Vehicle
Atlas V 521
Orbital Elements
NORAD ID
28472
International Designator
2004-048A
Epoch
Sat, 04 Jul 2026 03:13:36 GMT
Apogee
Calculating...
Perigee
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Inclination
4.64°
Right Ascension
76.24°
Eccentricity
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Argument of Perigee
209.22°
Period
1453.02 min
Mean Motion
0.99 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
AMC-16
Alternative Name
AMC 16
Type
Payload
Status
Non-operational
Owner
AMCS
Country
United States
Constellation
N/A
Related Satellites
Major Events
N/A
Latest TLEs
1 28472U 04048A 26185.13445125 -.00000055 00000-0 00000-0 0 9997
2 28472 4.6444 76.2364 0002741 209.2173 322.1131 0.99103748 78653
Source: Celestrak
Summary
AMC-16, also known as AMC 16 or Americom 16, is a communication satellite owned by AMCS and manufactured by LMCSS. Launched on December 17, 2004, from the Air Force Eastern Test Range (AFETR) SLC41 using an Atlas V 521 launch vehicle, it has a configuration of A2100AXS with dimensions including a length of 6 meters, diameter of 3.6 meters, and span of 26 meters. The satellite weighs 4,065 kg at launch and has a dry mass of 2,000 kg. It is equipped with 24 Ku-band transponders and 12 Ka-band transponder for communication purposes and uses two deployable solar arrays and batteries for power supply. Its mission lifetime was projected to be 15 years.
Physical Characteristics
Length
6
Diameter
3.6
Span
26
Dry Mass
2000
Launch Mass
4065
Shape
Box + 2 Pan
Radar Cross Section
7.9432
Visual Magnitude
Unknown
Color
Unknown
Material Composition
Unknown
Technical Details
Payload
Americom 16
Purpose
Communication
Mission
Communication
Manufacturer
LMCSS
Life Expectancy
15 years
Bus
A2100
Configuration
A2100AXS
Motor
Leros 1C
Equipment
24 Ku-band transponders, 12 Ka-band transponder
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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