STARLINK-32113 (60282)

COSPAR: 2024-132E | Alt Name: Starlink 32113

Image

Additional Sources

Launch Details

Launch Date

July 28, 2024

Launch Site

Cape Canaveral Space Force Station

Launch Pad

LC40

Launch Vehicle

Falcon 9

Orbital Elements

NORAD ID

60282

International Designator

2024-132E

Epoch

Mon, 20 Jul 2026 06:00:04 GMT

Apogee

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Perigee

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Inclination

53.16°

Right Ascension

156.48°

Eccentricity

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Argument of Perigee

73.76°

Period

93.85 min

Mean Motion

15.34 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

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Starlink V2M bus SpaceX Starlink constellation United States satellites Payloads

Basic Satellite Info

Name

STARLINK-32113

Alternative Name

Starlink 32113

Type

Payload

Status

Operational

Owner

SPXS

Country

United States

Constellation

N/A

Related Satellites

Major Events

N/A

Latest TLEs

1 60282U 24132E   26201.25004630  .00032597  00000+0  97246-3 0  9997

2 60282  53.1606 156.4838 0001324  73.7603 122.2424 15.34375254  5867

Source: Celestrak

Summary

STARLINK-32113 is a Starlink v2 Mini satellite (BUS: Starlink V2M) owned and operated by SPXS. Launched on July 28, 2024, from Cape Canaveral Air Force Station LC40 using a Falcon 9 launch vehicle, the satellite has dimensions of 0.3 meters in length with a diameter of 4.1 meters and a span of 29 meters. It weighs 730 kilograms at launch and has a dry mass of 700 kilograms. The satellite is equipped with Ku/Ka/E-band payload and an optical inter-satellite link for communication purposes, powered by solar arrays and batteries. Its propulsion system consists of Argon ion thrusters, designed for the Starlink Group 10-4-05 mission to enhance global communication capabilities.

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 10-4-05

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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