STARLINK-32193 (60428)

COSPAR: 2024-144D | Alt Name: Starlink 32193

Image
STARLINK-32193 Satellite Image
Additional Sources
Launch Details

Launch Date

August 12, 2024

Launch Pad

LC39A

Launch Vehicle

Falcon 9

Orbital Elements

NORAD ID

60428

International Designator

2024-144D

Epoch

Sun, 19 Jul 2026 09:08:05 GMT

Apogee

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Perigee

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Inclination

53.16°

Right Ascension

324.60°

Eccentricity

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Argument of Perigee

100.25°

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-32193

Alternative Name

Starlink 32193

Type

Payload

Status

Operational

Owner

SPXS

Country

United States

Constellation

N/A

Related Satellites

Major Events

N/A

Latest TLEs
1 60428U 24144D   26200.38062047  .00001370  00000+0  51688-4 0  9997
2 60428  53.1593 324.5950 0000919 100.2476 259.8630 15.34387871109522

Source: Celestrak

Summary
STARLINK-32193, also known as Starlink 32193, is a communication satellite belonging to the Starlink v2 Mini configuration and part of the Starlink Group 10-7-04 payload. It was launched on August 12, 2024, from LC39A at AFETR 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. Its dry mass is 700 kg, while its launch mass was 730 kg. It features an equipment payload that includes Ku/Ka/E-band communication capabilities along with optical inter-satellite links. Power is supplied through solar arrays and batteries, and it uses Argon ion thrusters for propulsion. The satellite's shape is described as a box with panels. Manufactured by SPXS (SpaceX), the mission of STARLINK-32193 is to enhance communication services as part of SpaceX’s larger constellation effort.

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 10-7-04

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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