IRIDIUM 83 (25531)

COSPAR: 1998-066E | Alt Name: Iridium 83
DECAYED

Image
IRIDIUM 83 Satellite Image
Additional Sources
Launch Details

Launch Date

November 6, 1998

Launch Site

AFWTR

Launch Pad

SLC2W

Launch Vehicle

Delta 7920-10C

Orbital Elements

NORAD ID

25531

International Designator

1998-066E

Decay Date

11/5/2018

Basic Satellite Info

Name

IRIDIUM 83

Alternative Name

Iridium 83

Type

Payload

Status

Decayed

Owner

IRID

Country

United States

Constellation

N/A

Related Satellites

Major Events

N/A

Summary
IRIDIUM 83, also known as Iridium SV083, is a communication satellite built by MOTO/LMMS and launched on November 6, 1998, from AFWTR using the Delta 7920-10C launch vehicle. It has a configuration of LM-700A with dimensions of 3.5 meters in length, 1 meter in diameter, and a span of 5 meters. The satellite's dry mass is 556 kg, and it was launched with a total mass of 662 kg. Its power system includes two deployable solar arrays and batteries. It has a shape described as "Box + 2 Pan" and a radar cross-section (RCS) value of 3.91 square meters. The satellite's mission is communication, and it was operational for an expected lifetime of 8 years. It is owned by IRID and operates within the Iridium constellation.
Physical Characteristics

Length

3.5

Diameter

1

Span

5

Dry Mass

556

Launch Mass

662

Shape

Box + 2 Pan

Radar Cross Section

3.91

Visual Magnitude

Unknown

Color

Unknown

Material Composition

Unknown

Technical Details

Payload

Iridium SV083

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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