STARLINK-32134 (60300)

COSPAR: 2024-132Y | Alt Name: Starlink 32134

Image
STARLINK-32134 Satellite Image
Additional Sources
Launch Details

Launch Date

July 28, 2024

Launch Pad

LC40

Launch Vehicle

Falcon 9

Orbital Elements

NORAD ID

60300

International Designator

2024-132Y

Epoch

Mon, 20 Jul 2026 06:27:40 GMT

Apogee

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Perigee

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Inclination

53.16°

Right Ascension

156.28°

Eccentricity

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Argument of Perigee

59.60°

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
Basic Satellite Info

Name

STARLINK-32134

Alternative Name

Starlink 32134

Type

Payload

Status

Operational

Owner

SPXS

Country

United States

Constellation

N/A

Related Satellites

Major Events

N/A

Latest TLEs
1 60300U 24132Y   26201.26921311 -.00001128  00000+0 -22253-4 0  9998
2 60300  53.1619 156.2770 0001291  59.6042 300.5089 15.34397944111864

Source: Celestrak

Summary
STARLINK-32134, also known as Starlink 32134, is a communication satellite belonging to SpaceX (SPXS). Launched on July 28, 2024, from Cape Canaveral Air Force Station's LC40 pad using a Falcon 9 launch vehicle, it is part of the Starlink v2 Mini configuration under the Starlink V2M bus type. The satellite measures 0.3 meters in length and has a diameter of 4.1 meters with a span of 29 meters, indicating its solar arrays or antennas deployment size. It weighs 700 kilograms dry and was launched at 730 kilograms. Equipped with Ku/Ka/E-band payload capabilities along with optical inter-satellite links, it uses Argon ion thrusters for maneuvering and is powered by solar arrays and batteries. The satellite's primary mission is to provide 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

29

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 10-4-23

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

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