IRIDIUM 6 (24794)

COSPAR: 1997-020C | Alt Name: Iridium 6
DECAYED

Image
IRIDIUM 6 Satellite Image
Additional Sources
Launch Details

Launch Date

May 5, 1997

Launch Site

AFWTR

Launch Pad

SLC2W

Launch Vehicle

Delta 7920-10C

Orbital Elements

NORAD ID

24794

International Designator

1997-020C

Decay Date

12/23/2017

Basic Satellite Info

Name

IRIDIUM 6

Alternative Name

Iridium 6

Type

Payload

Status

Decayed

Owner

IRID

Country

United States

Constellation

N/A

Related Satellites

Major Events

N/A

Summary
IRIDIUM 6 is a communication satellite launched by Iridium LLC on May 5, 1997, from Vandenberg Air Force Base using a Delta 7920-10C launch vehicle. The spacecraft measures 3.5 meters in length with a diameter of 1 meter and a span of 5 meters. It has a dry mass of 556 kg and was launched with a total mass of 662 kg. IRIDIUM 6 is part of the LM-700A configuration based on the LM700 bus, manufactured by MOTO/LMMS for communication purposes. The satellite's power system includes two deployable solar arrays and batteries. Its shape consists of a box with two panels and has an RCS (Reaction Control System) value of 3.2266. The mission lifespan was expected to be around 8 years, with the primary purpose being to facilitate global communication services as part of the Iridium constellation system.
Physical Characteristics

Length

3.5

Diameter

1

Span

5

Dry Mass

556

Launch Mass

662

Shape

Box + 2 Pan

Radar Cross Section

3.2266

Visual Magnitude

Unknown

Color

Unknown

Material Composition

Unknown

Technical Details

Payload

Iridium SV006

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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