IRIDIUM 111 (41926)

COSPAR: 2017-003K | Alt Name: Iridium Next SV111

Image
IRIDIUM 111 Satellite Image
Additional Sources
Launch Details

Launch Date

January 14, 2017

Launch Site

AFWTR

Launch Pad

SLC4E

Launch Vehicle

Falcon 9

Orbital Elements

NORAD ID

41926

International Designator

2017-003K

Epoch

Sat, 04 Jul 2026 03:27:54 GMT

Apogee

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Perigee

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Inclination

86.40°

Right Ascension

81.29°

Eccentricity

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Argument of Perigee

83.58°

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 111

Alternative Name

Iridium Next SV111

Type

Payload

Status

Operational

Owner

IRIDS

Country

United States

Constellation

N/A

Related Satellites

Major Events

N/A

Latest TLEs
1 41926U 17003K   26185.14437653  .00000116  00000-0  34316-4 0  9997
2 41926  86.3954  81.2881 0002171  83.5770 276.5673 14.34217358495684

Source: Celestrak

Summary
IRIDIUM 111, also known as Iridium Next SV111, is a communication and traffic monitoring satellite manufactured by OATKGA for IRIDS (Iridium). Launched on January 14, 2017, from AFWTR SLC4E using a Falcon 9 launch vehicle, the satellite has dimensions of 3.1 meters in length, 1.5 meters in diameter, and spans 9.4 meters with its deployable solar arrays and batteries for power supply. It weighs 860 kg at launch and is designed to have an operational lifespan of up to 15 years. The satellite's configuration includes L-band payload, Ka-band cross-links and downlinks, as well as ADS-B payload and AIS-receiver capabilities. Its shape is described as a half hex prism with two panels, and it has a radar cross-section (RCS) value of 2.6291 square meters.
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

2.6291

Visual Magnitude

Unknown

Color

Unknown

Material Composition

Unknown

Technical Details

Payload

Iridium Next SV111

Purpose

Communication, traffic monitoring

Mission

Communication, traffic monitoring

Manufacturer

OATKGA

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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