NAVSTAR 23 (USA 71) (21552)

COSPAR: 1991-047A | Alt Name: GPS IIA-2

Image
NAVSTAR 23 (USA 71) Satellite Image
Additional Sources
Launch Details

Launch Date

July 4, 1991

Launch Pad

LC17A

Launch Vehicle

Delta 7925

Orbital Elements

NORAD ID

21552

International Designator

1991-047A

Epoch

Wed, 01 Jul 2026 15:49:33 GMT

Apogee

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Perigee

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Inclination

56.51°

Right Ascension

352.06°

Eccentricity

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Argument of Perigee

134.62°

Period

750.55 min

Mean Motion

1.92 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

NAVSTAR 23 (USA 71)

Alternative Name

GPS IIA-2

Type

Payload

Status

Non-operational

Owner

AFSSD2

Country

United States

Constellation

N/A

Related Satellites

Major Events

N/A

Latest TLEs
1 21552U 91047A   26182.65941149 -.00000086  00000-0  00000-0 0  9999
2 21552  56.5137 352.0599 0034449 134.6159  41.7572  1.91858562251661

Source: Celestrak

Summary
NAVSTAR 23 (USA 71), also known as GPS IIA-2, is a satellite within the GPS constellation and was launched on July 4, 1991, from Cape Canaveral Air Force Station's Launch Complex 17A using a Delta 7925 launch vehicle. It has dimensions of 2.4 meters in length, 1.8 meters in diameter, and a span of 5.3 meters when its solar arrays are deployed. The satellite features a 3-Axis stabilization system for navigation purposes and was manufactured by RWISB. With a dry mass of 860 kilograms, it carries the GPS SVN 24 payload and is powered by two deployable solar arrays along with batteries. Its mission involves providing global positioning services, and it has an expected lifetime of approximately 7.5 years.
Physical Characteristics

Length

2.4

Diameter

1.8

Span

5.3

Dry Mass

860

Launch Mass

860

Shape

Box + 2 Pan

Radar Cross Section

3.9045

Visual Magnitude

Unknown

Color

Unknown

Material Composition

Unknown

Technical Details

Payload

GPS SVN 24

Purpose

Navigation

Mission

Navigation

Manufacturer

RWISB

Life Expectancy

7.5 years

Bus

GPS IIA

Configuration

3-Axis stabilized

Motor

Star 37XFP

Equipment

?

Power System

2 deployable solar arrays, batteries

ADCS

Unknown

Transmitter Frequency

Unknown

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