IRIDIUM 129 (42958)

COSPAR: 2017-061D | Alt Name: Iridium Next SV129

Image
IRIDIUM 129 Satellite Image
Additional Sources
Launch Details

Launch Date

October 9, 2017

Launch Site

AFWTR

Launch Pad

SLC4E

Launch Vehicle

Falcon 9

Orbital Elements

NORAD ID

42958

International Designator

2017-061D

Epoch

Sat, 04 Jul 2026 06:02:26 GMT

Apogee

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Perigee

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Inclination

86.40°

Right Ascension

18.12°

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 129

Alternative Name

Iridium Next SV129

Type

Payload

Status

Operational

Owner

IRIDS

Country

United States

Constellation

N/A

Related Satellites

Major Events

N/A

Latest TLEs
1 42958U 17061D   26185.25169661  .00000236  00000-0  77358-4 0  9996
2 42958  86.3964  18.1177 0002259  83.5800 276.5654 14.34219187457240

Source: Celestrak

Summary
IRIDIUM 129, also known as Iridium Next SV129, is a communication and traffic monitoring satellite operated by IRIDS (Iridium). It was launched on October 9, 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 a span of 9.4 meters. It features an EliteBus configuration with a dry mass of 700 kilograms and a launch mass of 860 kilograms. Equipped with L-band payload, Ka-band cross-links, downlinks, ADS-B payload, and AIS-receiver, the satellite is designed for a 10-year mission but planned to operate for up to 15 years. Its power system consists of two deployable solar arrays and batteries, and it has a half hex prism+2 pan shape.
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 SV129

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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