IRIDIUM 47 (25106)

COSPAR: 1997-082C | Alt Name: Iridium 47

DECAYED

Image

Additional Sources

Launch Details

Launch Date

December 20, 1997

Launch Site

AFWTR

Launch Pad

SLC2W

Launch Vehicle

Delta 7920-10C

Orbital Elements

NORAD ID

25106

International Designator

1997-082C

Decay Date

9/1/2018

Basic Satellite Info

Name

IRIDIUM 47

Alternative Name

Iridium 47

Type

Payload

Status

Decayed

Owner

IRID

Country

United States

Constellation

N/A

Related Satellites

Major Events

N/A

Summary

IRIDIUM 47 is a communication satellite launched by the United States on December 20, 1997, from Vandenberg Air Force Base using a Delta 7920-10C launch vehicle. It measures 3.5 meters in length with a diameter of 1 meter and spans 5 meters when its solar arrays are deployed. The satellite has a dry mass of 556 kilograms and weighed 662 kilograms at launch. It was manufactured by MOTO/LMMS, based on the LM-700A configuration, and is part of the Iridium constellation for communication purposes. IRIDIUM 47 is equipped with two deployable solar arrays and batteries to power its operations and has a lifespan of approximately eight years. The satellite's shape consists of a box design with two panels and it carries the payload known as Iridium SV047.

Physical Characteristics

Length

3.5

Diameter

Span

Dry Mass

556

Launch Mass

662

Shape

Box + 2 Pan

Radar Cross Section

3.3188

Visual Magnitude

Unknown

Color

Unknown

Material Composition

Unknown

Technical Details

Payload

Iridium SV047

Purpose

Communication

Mission

Communication

Manufacturer

MOTO/LMMS

Life Expectancy

8 years

Bus

LM700

Configuration

LM-700A

Motor

Equipment

Power System

2 deployable solar arrays, batteries

ADCS

Unknown

Transmitter Frequency

Unknown

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