USA 134 (25019)

COSPAR: 1997-065A | Alt Name: DSCS III B-13

Image
USA 134 Satellite Image
Additional Sources
Launch Details

Launch Date

October 25, 1997

Launch Pad

LC36A

Launch Vehicle

Atlas IIA

Orbital Elements

NORAD ID

25019

International Designator

1997-065A

Epoch

Sat, 04 Jul 2026 03:05:07 GMT

Apogee

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Perigee

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Inclination

12.80°

Right Ascension

21.59°

Eccentricity

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Argument of Perigee

344.90°

Period

1436.10 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 134

Alternative Name

DSCS III B-13

Type

Payload

Status

Operational

Owner

AFSMC/DISA

Country

United States

Constellation

N/A

Related Satellites

Major Events

N/A

Latest TLEs
1 25019U 97065A   26185.12855789 -.00000055  00000-0  00000-0 0  9992
2 25019  12.8029  21.5904 0002467 344.9001 209.4956  1.00271697 33129

Source: Celestrak

Summary
The USA 134 satellite, also known as DSCS III B-13, is a communication satellite owned by AFSMC/DISA and manufactured by LMVF. Launched on October 25, 1997, from Launch Complex 36A at Cape Canaveral Air Force Station using an Atlas IIA launch vehicle, it has a configuration based on the DSCS-3 Bus with 3-axis stabilization. The satellite measures 2.1 meters in length and 1.9 meters in diameter with a span of 9.5 meters, weighing 1232 kg at launch and having a dry mass of 900 kg. It is equipped with 6 SHF transponders and 1 special purpose transponder (SHF and UHF), powered by two deployable solar arrays and batteries. The satellite's shape consists of a box with two panels. Its mission, lasting approximately 10 years, focused on communication purposes for the US military.
Physical Characteristics

Length

2.1

Diameter

1.9

Span

9.5

Dry Mass

900

Launch Mass

1232

Shape

Box + 2 Pan

Radar Cross Section

Unknown

Visual Magnitude

Unknown

Color

Unknown

Material Composition

Unknown

Technical Details

Payload

DSCS III B-13

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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