Official name MUOS 3
Alternative name MUOS 3
Cospar ID 2015-002A
Norad ID 40374
Launch date 2015-01-21
Launch site AFETR
Launch vehicle Atlas-5(551)¹
Country/Organization USA
Type application Comsat
Operator US Navy
RCS size LARGE
Decay date ON ORBIT
Period (min) 1436.12
Inclination (deg) 3.19
Perigee (km) 35565
Apogee (km) 36009
Eccentricity 0.00620336993880459
Mean motion (revs. per day) 1.00270172408991
Semi-Major axis (km) 42165.135
Raan (deg) 34.3942
Arg of perigee (deg) 178.6243
Shape Box + 2 Pan + 1 Dish
Mass (kg) 6800
Height (m) 7.9
Width (m) 4.3
Depth (m) 4.3
Span (m^2) 28.7
Lifetime 15 years
Contractors Lockheed Martin (Prime), Boeing, General Dynamics
Equipment ?
Propulsion IHI BT-4
Configuration A2100M
Power 2 deployable solar arrays, batteries

MUOS (Mobile User Objective System) is a next-generation narrowband tactical satellite communications system designed to significantly improve ground communications for U.S. forces on the move.

The new communications system, slated to become operational in 2010, would provide 10 times more throughput, or volume of information that can be transmitted, than the current UFO System, and will provide the US troops a much more reliable way to communicate, as it is not affected by weather, environmental constraints or foliage.

Under the new system, even troops in the most remote locations or buildings with no satellite access would see a big increase in communications capabilities, industry sources said.

In September 2004 the Lockheed team was selected against the Raytheon team.

Lockheed Martin Space Systems, Sunnyvale, Calif. the MUOS prime contractor and system integrator, was recently awarded a $2.1 billion contract to build the first two satellites and associated ground control elements by the U.S. Navy Space and Naval Warfare Systems Command (SPAWAR), on behalf of the Program Executive Office – Space Systems, San Diego, Calif. The contract also provides for options on three additional spacecraft. With all options exercised, the contract for up to five satellites has a total potential value of $3.26 billion.

MUOS satellites will be developed at the company's Commercial Space Systems unit in Newtown, Pa.; final assembly and test will occur in Sunnyvale. Lockheed Martin's award-winning A2100 bus, which has achieved over 100 years of on-orbit service, will serve as the MUOS spacecraft platform.

  • General Dynamics C4 Systems, Scottsdale, Ariz., which will lead the user-entry and integrated ground segments of the MUOS program, supplying a secure ground network, satellite control and network management, and a JTRS-compliant terminal solution.
  • Boeing Satellite Systems (BSS), El Segundo, Calif.; The satellite-manufacturing arm of Boeing Integrated Defense Systems will provide the legacy UHF payload.
  • Ericsson, Plano, Texas. The leader in 2G and 3G mobile technology systems will provide portions of the integrated ground segment.
  • Harris Corporation, Melbourne, Fla. A world leader in spaceborne, unfurlable mesh reflectors, Harris will provide the large reflectors for the MUOS program. The reflectors, two per satellite, will be manufactured at Harris facilities as part of the MUOS geo-synchronous satellite's ultra high-frequency (UHF)-band antenna system.

The planned launch of the first MUOS satellite was delayed to 2012 after a part of the budget was used to fund operations in Iraq.

The program is valued at $6.4 billion over its lifespan, which could run through 2024.

In 2014, in the third MUOS a soldering defect was discovered, shuffling it behind the fourth spacecraft in the five-member fleet.

MUOS 5, launched in June 2016, suffered issues with its apogee propulsion system during orbit raising and has not raised its orbit to the final geostationary orbit but stayed in an intermediate transfer orbit. Between 7 September and 22 October 2016, a total of 26 firings by the smaller, less powerful thrusters lifted MUOS 5 to a synchronous orbit and thus salvaging the mission.

Satellite COSPAR Date LS Launch Vehicle Remarks
MUOS 1 2012-009A 2012-02-24 AFETR Atlas-5(551)¹
MUOS 2 2013-036A 2013-07-19 AFETR Atlas-5(551)¹
MUOS 3 2015-002A 2015-01-21 AFETR Atlas-5(551)¹
MUOS 4 2015-044A 2015-09-02 AFETR Atlas-5(551)¹
MUOS 5 2016-041A 2016-06-24 AFETR Atlas-5(551)¹