USA 167 (27691)

COSPAR: 2003-008A | Alt Name: DSCS III A-3

Image
USA 167 Satellite Image
Additional Sources
Launch Details

Launch Date

March 11, 2003

Launch Pad

SLC37B

Launch Vehicle

Delta 4M

Orbital Elements

NORAD ID

27691

International Designator

2003-008A

Epoch

Fri, 03 Jul 2026 06:26:38 GMT

Apogee

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Perigee

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Inclination

10.99°

Right Ascension

43.26°

Eccentricity

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Argument of Perigee

316.96°

Period

1436.09 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

USA 167

Alternative Name

DSCS III A-3

Type

Payload

Status

Operational

Owner

AFSMC/DISA

Country

United States

Constellation

N/A

Related Satellites

Major Events

N/A

Latest TLEs
1 27691U 03008A   26184.26850422  .00000010  00000-0  00000-0 0  9997
2 27691  10.9909  43.2613 0003348 316.9630 256.0432  1.00272289  6931

Source: Celestrak

Summary
The USA 167 satellite, also known as DSCS III A-3, is a communication satellite launched on March 11, 2003, from the Air Force Eastern Test Range (AFETR) using a Delta 4M launch vehicle. It has a configuration of a DSCS-3 bus with 3-axis stabilization and was manufactured by LMVF for the AFSMC/DISA. The satellite measures 2.1 meters in length, 1.9 meters in diameter, and its span is 9.5 meters. It had a launch mass of 1244 kilograms and a dry mass of 900 kilograms. Its communication equipment includes six SHF transponders and one special purpose transponder (SHF and UHF). Power is supplied by two deployable solar arrays and batteries. The satellite's shape is described as "Box + 2 Pan," with no additional information provided on its color, transmitter frequencies, or major events during its expected 10-year lifetime.
Physical Characteristics

Length

2.1

Diameter

1.9

Span

9.5

Dry Mass

900

Launch Mass

1244

Shape

Box + 2 Pan

Radar Cross Section

Unknown

Visual Magnitude

Unknown

Color

Unknown

Material Composition

Unknown

Technical Details

Payload

DSCS III A-3

Purpose

Communication

Mission

Communication

Manufacturer

LMVF

Life Expectancy

10 years

Bus

DSCS III

Configuration

DSCS-3 Bus, 3-Axis stabilization

Motor

AOCS

Equipment

6 SHF transponders, 1 special purpose transponder (SHF and UHF)

Power System

2 deployable solar arrays, batteries

ADCS

Unknown

Transmitter Frequency

Unknown

Map
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