IRIDIUM 120 (42805)

COSPAR: 2017-039C | Alt Name: Iridium Next SV120

Image
IRIDIUM 120 Satellite Image
Additional Sources
Launch Details

Launch Date

June 25, 2017

Launch Site

AFWTR

Launch Pad

SLC4E

Launch Vehicle

Falcon 9

Orbital Elements

NORAD ID

42805

International Designator

2017-039C

Epoch

Sat, 04 Jul 2026 02:49:54 GMT

Apogee

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Perigee

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Inclination

86.40°

Right Ascension

314.88°

Eccentricity

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Argument of Perigee

98.78°

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 120

Alternative Name

Iridium Next SV120

Type

Payload

Status

Operational

Owner

IRIDS

Country

United States

Constellation

N/A

Related Satellites

Major Events

N/A

Latest TLEs
1 42805U 17039C   26185.11799672  .00000209  00000-0  67647-4 0  9998
2 42805  86.3977 314.8818 0002267  98.7827 261.3625 14.34219564473606

Source: Celestrak

Summary
IRIDIUM 120, also known as Iridium Next SV120, is a communication and traffic monitoring satellite owned by IRIDS (Iridium). It was launched on June 25, 2017, from AFWTR SLC4E using a Falcon 9 launch vehicle. With dimensions of 3.1 meters in length, 1.5 meters in diameter, and a span of 9.4 meters, the satellite has a dry mass of 700 kg and launched with a total mass of 860 kg. Equipped with an L-band payload, Ka-band cross-links and downlinks, ADS-B payload, and AIS-receiver (part of a fleet of 58 satellites), IRIDIUM 120 is powered by two deployable solar arrays and batteries. Its design life expectancy is 10 years, though it is planned to operate for up to 15 years. The satellite has a configuration known as ELiTeBus-1000 and was manufactured by OATKGA (Other Aerospace Technologies & Knowledge Generating Agency).
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 SV120

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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