IRIDIUM 20 (25577)

COSPAR: 1998-074A | Alt Name: Iridium 20A
DECAYED

Image
IRIDIUM 20 Satellite Image
Additional Sources
Launch Details

Launch Date

December 19, 1998

Launch Site

TAISC

Launch Pad

LC7

Launch Vehicle

Chang Zheng 2C-III/SD

Orbital Elements

NORAD ID

25577

International Designator

1998-074A

Decay Date

10/22/2018

Basic Satellite Info

Name

IRIDIUM 20

Alternative Name

Iridium 20A

Type

Payload

Status

Decayed

Owner

IRID

Country

United States

Constellation

N/A

Related Satellites

Major Events

N/A

Summary
IRIDIUM 20 (also known as Iridium 20A) is a communication satellite with NORAD Catalog ID 25577 and OBJECT_ID 1998-074A, manufactured by MOTO under the LM700 BUS configuration. Launched on December 19, 1998, from Taiyuan Satellite Launch Center (TAISC) using a Chang Zheng 2C-III/SD launch vehicle, it has dimensions of 3.5 meters in length and 1 meter in diameter with a span of 5 meters. The satellite's dry mass is 556 kg, and its launch mass was 667 kg. It uses two deployable solar arrays and batteries for power generation. The satellite's shape is described as Box + 2 Pan with an RCS of 3.6949 m². Its mission is to provide communication services, operating in a low Earth orbit with an expected lifetime of 8 years.
Physical Characteristics

Length

3.5

Diameter

1

Span

5

Dry Mass

556

Launch Mass

667

Shape

Box + 2 Pan

Radar Cross Section

3.6949

Visual Magnitude

Unknown

Color

Unknown

Material Composition

Unknown

Technical Details

Payload

Iridium SV088

Purpose

Communication

Mission

Communication

Manufacturer

MOTO

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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