IRIDIUM 98 (27451)

COSPAR: 2002-031B | Alt Name: Iridium 98
DECAYED

Image
IRIDIUM 98 Satellite Image
Additional Sources
Launch Details

Launch Date

June 20, 2002

Launch Site

PLMSC

Launch Pad

LC133/3

Launch Vehicle

Rokot

Orbital Elements

NORAD ID

27451

International Designator

2002-031B

Decay Date

8/24/2018

Basic Satellite Info

Name

IRIDIUM 98

Alternative Name

Iridium 98

Type

Payload

Status

Decayed

Owner

IRIDS

Country

United States

Constellation

N/A

Related Satellites

Major Events

N/A

Summary
IRIDIUM 98, also known as Iridium SV098, is a communication satellite launched on June 20, 2002, from PLMSC Launch Site LC133/3 using the Rokot launch vehicle. It was manufactured by MOTO and belongs to IRIDS. With dimensions of 3.5 meters in length, 1 meter in diameter, and a span of 5 meters, it has a dry mass of 556 kilograms and a launch mass of 655 kilograms. The satellite uses two deployable solar arrays for power generation along with batteries to support its mission requirements. Its shape is described as Box + 2 Pan with an RCS of 3.3916 square meters, and it was designed with the LM-700A configuration based on the LM700 bus. The satellite's motor is Primex EHT, and it has a planned lifetime of eight years for its communication mission.
Physical Characteristics

Length

3.5

Diameter

1

Span

5

Dry Mass

556

Launch Mass

655

Shape

Box + 2 Pan

Radar Cross Section

3.3916

Visual Magnitude

Unknown

Color

Unknown

Material Composition

Unknown

Technical Details

Payload

Iridium SV098

Purpose

Communication

Mission

Communication

Manufacturer

MOTO

Life Expectancy

8 years

Bus

LM700

Configuration

LM-700A

Motor

Primex EHT

Equipment

?

Power System

2 deployable solar arrays, batteries

ADCS

Unknown

Transmitter Frequency

Unknown

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