IRIDIUM 176 (43923)

COSPAR: 2019-002B | Alt Name: Iridium Next SV176

Image
IRIDIUM 176 Satellite Image
Additional Sources
Launch Details

Launch Date

January 11, 2019

Launch Site

AFWTR

Launch Pad

SLC4E

Launch Vehicle

Falcon 9

Orbital Elements

NORAD ID

43923

International Designator

2019-002B

Epoch

Sat, 04 Jul 2026 03:37:23 GMT

Apogee

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Perigee

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Inclination

86.61°

Right Ascension

346.45°

Eccentricity

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Argument of Perigee

88.22°

Period

97.81 min

Mean Motion

14.72 rev/day

Latitude

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Longitude

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Altitude

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Velocity

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Polar Plot
3D Visualization
Basic Satellite Info

Name

IRIDIUM 176

Alternative Name

Iridium Next SV176

Type

Payload

Status

Operational

Owner

IRIDS

Country

United States

Constellation

N/A

Related Satellites

Major Events

N/A

Latest TLEs
1 43923U 19002B   26185.15096466  .00000924  00000-0  14274-3 0  9998
2 43923  86.6101 346.4461 0002366  88.2178 271.9310 14.72237889401744

Source: Celestrak

Summary
IRIDIUM 176, also known as Iridium Next SV176, is a communication and traffic monitoring satellite launched on January 11, 2019, from Vandenberg Air Force Base (AFWTR) using Falcon 9 as the launch vehicle. It was manufactured by NGISGA and owned by IRIDS. The satellite measures 3.1 meters in length with a diameter of 1.5 meters and a span of 9.4 meters. It has a dry mass of 700 kg and a launch mass of 860 kg, featuring a configuration known as ELiTeBus-1000. Its equipment includes an L-band payload, Ka-band cross-links and downlinks, ADS-B payload, and AIS-receiver. The satellite is powered by two deployable solar arrays and batteries. It has a design lifetime of 10 years but plans are set for it to operate up to 15 years.
Physical Characteristics

Length

3.1

Diameter

1.5

Span

9.4

Dry Mass

700

Launch Mass

860

Shape

Half Hex Prism+2 pan

Radar Cross Section

Unknown

Visual Magnitude

Unknown

Color

Unknown

Material Composition

Unknown

Technical Details

Payload

Iridium Next SV176

Purpose

Communication, traffic monitoring

Mission

Communication, traffic monitoring

Manufacturer

NGISGA

Life Expectancy

10 years (design), 15 years (planned)

Bus

EliteBus

Configuration

ELiTeBus-1000

Motor

?

Equipment

L-band payload, Ka-band cross-links, Ka-band downlinks, ADS-B payload, AIS-receiver (on 58 satellites)

Power System

2 deployable solar arrays, batteries

ADCS

Unknown

Transmitter Frequency

Unknown

Map
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