IRIDIUM 14 (25777)

COSPAR: 1999-032A | Alt Name: Iridium 14A
DECAYED

Image
IRIDIUM 14 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

25777

International Designator

1999-032A

Decay Date

3/15/2019

Basic Satellite Info

Name

IRIDIUM 14

Alternative Name

Iridium 14A

Type

Payload

Status

Decayed

Owner

IRID

Country

United States

Constellation

N/A

Related Satellites

Major Events

N/A

Summary
IRIDIUM 14 is a communication satellite with the OBJECT_ID 1999-032A and NORAD_CAT_ID 25777, manufactured by MOTO under the LM-700A configuration of the LM700 bus. It was launched on June 11, 1999, from the Taiyuan Satellite Launch Center (TAISC), LC7 launch pad, using a Chang Zheng 2C-III/SD launch vehicle. The satellite has dimensions of 3.5 meters in length, 1 meter in diameter, and a span of 5 meters. It had a dry mass of 556 kg and was launched with a mass of 655 kg. Its primary mission is communication, powered by two deployable solar arrays and batteries. The satellite's shape is described as a Box + 2 Pan with an RCS value of 3.2138. It has a lifetime expectancy of 8 years and is owned by IRID (Iridium LLC), carrying the payload Iridium SV092.
Physical Characteristics

Length

3.5

Diameter

1

Span

5

Dry Mass

556

Launch Mass

655

Shape

Box + 2 Pan

Radar Cross Section

3.2138

Visual Magnitude

Unknown

Color

Unknown

Material Composition

Unknown

Technical Details

Payload

Iridium SV092

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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