IRIDIUM 46 (24905)

COSPAR: 1997-043C | Alt Name: Iridium 24
DECAYED

Image
IRIDIUM 46 Satellite Image
Additional Sources
Launch Details

Launch Date

August 21, 1997

Launch Site

AFWTR

Launch Pad

SLC2W

Launch Vehicle

Delta 7920-10C

Orbital Elements

NORAD ID

24905

International Designator

1997-043C

Decay Date

5/11/2019

Basic Satellite Info

Name

IRIDIUM 46

Alternative Name

Iridium 24

Type

Payload

Status

Decayed

Owner

IRID

Country

United States

Constellation

N/A

Related Satellites

Major Events

N/A

Summary
IRIDIUM 46, also known as Iridium 24, is a communication satellite identified by NORAD CAT ID 24905 and OBJECT ID 1997-043C. It was launched on August 21, 1997, from the AFWTR launch site at SLC2W using a Delta 7920-10C launch vehicle. The satellite is based on the LM-700A configuration and manufactured by MOTO/LMMS for IRID (Iridium LLC). With dimensions of 3.5 meters in length, 1 meter in diameter, and a span of 5 meters, its dry mass is 556 kg while it had an initial launch mass of 662 kg. The satellite's power comes from two deployable solar arrays and batteries, and its shape consists of a box with two panels. IRIDIUM 46 has a designed lifetime of 8 years and serves as part of the Iridium constellation for communication purposes.
Physical Characteristics

Length

3.5

Diameter

1

Span

5

Dry Mass

556

Launch Mass

662

Shape

Box + 2 Pan

Radar Cross Section

3.4756

Visual Magnitude

Unknown

Color

Unknown

Material Composition

Unknown

Technical Details

Payload

Iridium SV024

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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