STARLINK-32175 (60339)

COSPAR: 2024-136L | Alt Name: Starlink 32175

Image

Additional Sources

Launch Details

Launch Date

August 2, 2024

Launch Site

Cape Canaveral Space Force Station

Launch Pad

LC39A

Launch Vehicle

Falcon 9

Orbital Elements

NORAD ID

60339

International Designator

2024-136L

Epoch

Sun, 19 Jul 2026 16:30:14 GMT

Apogee

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Perigee

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Inclination

53.16°

Right Ascension

182.58°

Eccentricity

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Argument of Perigee

84.62°

Period

94.11 min

Mean Motion

15.30 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

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Starlink V2M bus SpaceX Starlink constellation United States satellites Payloads

Basic Satellite Info

Name

STARLINK-32175

Alternative Name

Starlink 32175

Type

Payload

Status

Operational

Owner

SPXS

Country

United States

Constellation

N/A

Related Satellites

Major Events

N/A

Latest TLEs

1 60339U 24136L   26200.68767302 -.00000027  00000+0  11228-4 0  9993

2 60339  53.1600 182.5770 0001398  84.6244 275.4917 15.30195131109876

Source: Celestrak

Summary

The STARLINK-32175 satellite, also known as Starlink 32175, is a communication satellite built by SpaceX (SPXS). It was launched on August 2, 2024, from Launch Complex 39A at the Kennedy Space Center using a Falcon 9 launch vehicle. The satellite has dimensions of 0.3 meters in length and 4.1 meters in diameter with a span of 29 meters. It weighs approximately 700 kg dry and had a launch mass of 730 kg. Equipped with Ku/Ka/E-band payload, optical inter-satellite link, and Argon ion thrusters for propulsion, the satellite uses solar arrays and batteries for power. Its design is part of the Starlink v2 Mini configuration under the Starlink Group 10-6-11 payload category, aimed at providing communication services.

Starlink is a satellite constellation developed by SpaceX with the aim of providing global broadband internet coverage. Thousands of small satellites are deployed in low Earth orbit (LEO), enabling high-speed internet access even in remote areas. However, the rapid increase in satellites raises concerns about space debris and the potential for collisions, which can lead to further debris creation and endanger other spacecraft. Additionally, the sheer number of Starlink satellites can affect astronomical observations by increasing light pollution. Proper deorbiting plans and international coordination are essential to mitigate these challenges and ensure long-term sustainability in space.

Physical Characteristics

Length

0.3

Diameter

4.1

Span

Dry Mass

700

Launch Mass

730

Shape

Box + pan

Radar Cross Section

Unknown

Visual Magnitude

Unknown

Color

Unknown

Material Composition

Unknown

Technical Details

Payload

Starlink Group 10-6-11

Purpose

Communication

Mission

Communication

Manufacturer

SPXS

Life Expectancy

Unknown

Bus

Starlink V2M

Configuration

Starlink v2 Mini

Motor

Argon ion thrusters

Equipment

Ku/Ka/E-band payload, optical inter-satellite link

Power System

Solar arrays, batteries

ADCS

Unknown

Transmitter Frequency

Unknown

Map

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