IRIDIUM 168 (43924)

COSPAR: 2019-002C | Alt Name: Iridium Next SV168

Image
IRIDIUM 168 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

43924

International Designator

2019-002C

Epoch

Sat, 04 Jul 2026 03:40:30 GMT

Apogee

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Perigee

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Inclination

86.40°

Right Ascension

346.58°

Eccentricity

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Argument of Perigee

90.24°

Period

100.40 min

Mean Motion

14.34 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 168

Alternative Name

Iridium Next SV168

Type

Payload

Status

Operational

Owner

IRIDS

Country

United States

Constellation

N/A

Related Satellites

Major Events

N/A

Latest TLEs
1 43924U 19002C   26185.15313219  .00000034  00000-0  49842-5 0  9990
2 43924  86.3983 346.5819 0002209  90.2374 269.9075 14.34217533391403

Source: Celestrak

Summary
IRIDIUM 168, also known as Iridium Next SV168, is a satellite managed by IRIDS and manufactured by NGISGA. Launched on January 11, 2019, from AFWTR SLC4E using a Falcon 9 launch vehicle, this spacecraft has a configuration of ELiTeBus-1000 with dimensions measuring 3.1 meters in length, 1.5 meters in diameter, and spans 9.4 meters. It carries an L-band payload, Ka-band cross-links, downlinks, and ADS-B payload along with AIS-receivers on board. The satellite is designed for a lifetime of 10 years but plans extend its operation up to 15 years. Its primary mission involves communication and traffic monitoring, powered by two deployable solar arrays and batteries. The dry mass of IRIDIUM 168 is 700 kg, with an initial launch mass of 860 kg.
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 SV168

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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