STARLINK-32114 (60287)

COSPAR: 2024-132K | Alt Name: Starlink 32114

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

60287

International Designator

2024-132K

Epoch

Mon, 20 Jul 2026 06:24:59 GMT

Apogee

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Perigee

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Inclination

53.16°

Right Ascension

156.26°

Eccentricity

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Argument of Perigee

85.53°

Period

94.01 min

Mean Motion

15.32 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-32114

Alternative Name

Starlink 32114

Type

Payload

Status

Operational

Owner

SPXS

Country

United States

Constellation

N/A

Related Satellites

Major Events

N/A

Latest TLEs

1 60287U 24132K   26201.26735970  .00000115  00000+0  15477-4 0  9999

2 60287  53.1610 156.2641 0001507  85.5284 274.5890 15.31701348111866

Source: Celestrak

Summary

The STARLINK-32114 satellite, also known as Starlink 32114, is a communication satellite manufactured by SPXS and launched on July 28, 2024, from the Cape Canaveral Space Force Station (LC40) using a Falcon 9 launch vehicle. It belongs to the Starlink V2M bus with the configuration of Starlink v2 Mini. The satellite has dimensions of 0.3 meters in length and 4.1 meters in diameter, with a span of 29 meters. Its dry mass is 700 kilograms, and it was launched with a mass of 730 kilograms. Equipped with Ku/Ka/E-band payload and an optical inter-satellite link, the satellite uses Argon ion thrusters for propulsion and solar arrays along with batteries to generate power. It operates as part of the Starlink Group 10-4-10 constellation under the ownership of SPXS for communication purposes.

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 10-4-10

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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