IRIDIUM 18 (24872)

COSPAR: 1997-034D | Alt Name: Iridium 18
DECAYED

Image
IRIDIUM 18 Satellite Image
Additional Sources
Launch Details

Launch Date

July 9, 1997

Launch Site

AFWTR

Launch Pad

SLC2W

Launch Vehicle

Delta 7920-10C

Orbital Elements

NORAD ID

24872

International Designator

1997-034D

Decay Date

8/19/2018

Basic Satellite Info

Name

IRIDIUM 18

Alternative Name

Iridium 18

Type

Payload

Status

Decayed

Owner

IRID

Country

United States

Constellation

N/A

Related Satellites

Major Events

N/A

Summary
IRIDIUM 18 is a communication satellite, designated as 1997-034D, with the NORAD catalog ID of 24872. Launched on July 9, 1997, from AFWTR SLC2W using a Delta 7920-10C launch vehicle, it was manufactured by MOTO/LMMS and is part of the LM700 bus family with a configuration of LM-700A. The satellite has dimensions of 3.5 meters in length, a diameter of 1 meter, and a span of 5 meters. Its dry mass is 556 kilograms, and its launch mass was 662 kilograms. It is equipped with two deployable solar arrays and batteries for power generation. IRIDIUM 18 has an RCS (Reflective Cross Section) of 3.253 and a shape described as Box + 2 Pan. The satellite's purpose is communication, and it carries the payload Iridium SV018. Its expected operational lifetime was eight years.
Physical Characteristics

Length

3.5

Diameter

1

Span

5

Dry Mass

556

Launch Mass

662

Shape

Box + 2 Pan

Radar Cross Section

3.253

Visual Magnitude

Unknown

Color

Unknown

Material Composition

Unknown

Technical Details

Payload

Iridium SV018

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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