IRIDIUM 21 (25778)

COSPAR: 1999-032B | Alt Name: Iridium 21A
DECAYED

Image
IRIDIUM 21 Satellite Image
Additional Sources
Launch Details

Launch Date

June 11, 1999

Launch Site

TAISC

Launch Pad

LC7

Launch Vehicle

Chang Zheng 2C-III/SD

Orbital Elements

NORAD ID

25778

International Designator

1999-032B

Decay Date

5/24/2018

Basic Satellite Info

Name

IRIDIUM 21

Alternative Name

Iridium 21A

Type

Payload

Status

Decayed

Owner

IRID

Country

United States

Constellation

N/A

Related Satellites

Major Events

N/A

Summary
IRIDIUM 21, also known as Iridium 21A, is a communication satellite manufactured by MOTO and operated by IRID. It was launched on June 11, 1999, from the TISC launch site using the Chang Zheng 2C-III/SD vehicle from LC7. The satellite has a length of 3.5 meters, diameter of 1 meter, span of 5 meters, and a dry mass of 556 kg. It was equipped with two deployable solar arrays and batteries for power supply. IRIDIUM 21 is configured as LM-700A on the LM700 bus, has a mission lifetime of 8 years, and its motor type is Primex EHT. The satellite's shape is described as Box + 2 Pan with an RCS of 3.317.
Physical Characteristics

Length

3.5

Diameter

1

Span

5

Dry Mass

556

Launch Mass

655

Shape

Box + 2 Pan

Radar Cross Section

3.317

Visual Magnitude

Unknown

Color

Unknown

Material Composition

Unknown

Technical Details

Payload

Iridium SV093

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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