IRIDIUM 31 (24950)

COSPAR: 1997-051G | Alt Name: Iridium 31
DECAYED

Image
IRIDIUM 31 Satellite Image
Additional Sources
Launch Details

Launch Date

September 14, 1997

Launch Pad

LC81/23

Launch Vehicle

Proton-K/17S40

Orbital Elements

NORAD ID

24950

International Designator

1997-051G

Decay Date

12/20/2018

Basic Satellite Info

Name

IRIDIUM 31

Alternative Name

Iridium 31

Type

Payload

Status

Decayed

Owner

IRID

Country

United States

Constellation

N/A

Related Satellites

Major Events

N/A

Summary
IRIDIUM 31 is a communication satellite with the NORAD catalog ID of 24950 and OBJECT_ID 1997-051G, manufactured by MOTO/LMMS in the US. Launched on September 14, 1997, from TYMSC LC81/23 using a Proton-K/17S40 launch vehicle, this LM700 satellite has a configuration of LM-700A and is equipped with two deployable solar arrays and batteries for power. The satellite's dimensions are 3.5 meters in length, 1 meter in diameter, and spans 5 meters, with a dry mass of 556 kilograms and an initial launch mass of 662 kilograms. Its shape consists of a box structure plus two panels, and it has a reflectivity cross-section (RCS) of 3.5519 m². The mission's purpose is communication, with a lifetime expectancy of 8 years.
Physical Characteristics

Length

3.5

Diameter

1

Span

5

Dry Mass

556

Launch Mass

662

Shape

Box + 2 Pan

Radar Cross Section

3.5519

Visual Magnitude

Unknown

Color

Unknown

Material Composition

Unknown

Technical Details

Payload

Iridium SV031

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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