USA 44 (20203)

COSPAR: 1989-069B | Alt Name: DSCS III A-2

Image
USA 44 Satellite Image
Additional Sources
Launch Details

Launch Date

September 4, 1989

Launch Pad

LC40

Launch Vehicle

Titan 34D/Transtage

Orbital Elements

NORAD ID

20203

International Designator

1989-069B

Epoch

Fri, 03 Jul 2026 23:48:04 GMT

Apogee

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Perigee

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Inclination

14.72°

Right Ascension

3.94°

Eccentricity

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Argument of Perigee

24.37°

Period

1452.82 min

Mean Motion

0.99 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 44

Alternative Name

DSCS III A-2

Type

Payload

Status

Unknown

Owner

AFSSD2/DCA

Country

United States

Constellation

N/A

Related Satellites

Major Events

N/A

Latest TLEs
1 20203U 89069B   26184.99172124 -.00000085  00000-0  00000-0 0  9999
2 20203  14.7246   3.9427 0010663  24.3717 167.5890  0.99117751 25157

Source: Celestrak

Summary
USA 44, also known as DSCS III A-2, is a communication satellite launched on September 4, 1989, from Launch Complex 40 at the Air Force Eastern Test Range (AFETR) using a Titan 34D/Transtage launch vehicle. Manufactured by GEVF, it has a configuration of DSCS-3 Bus with 3-Axis stabilization and measures 2.1 meters in length, 1.9 meters in diameter, and spans 9.5 meters. The satellite had a dry mass of 876 kg and a launch mass of 1148 kg. It is equipped with 6 SHF transponders and 1 special purpose transponder for SHF and UHF communications. Its power source includes two deployable solar arrays and batteries, designed to operate in space for approximately ten years as part of the US Air Force Space Systems Directorate (AFSSD2/DCA) communication mission.
Physical Characteristics

Length

2.1

Diameter

1.9

Span

9.5

Dry Mass

876

Launch Mass

1148

Shape

Box + 2 Pan

Radar Cross Section

Unknown

Visual Magnitude

Unknown

Color

Unknown

Material Composition

Unknown

Technical Details

Payload

DSCS III A-2

Purpose

Communication

Mission

Communication

Manufacturer

GEVF

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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