STARLINK-32183 (60433)

COSPAR: 2024-144J | Alt Name: Starlink 32183

Image
STARLINK-32183 Satellite Image
Additional Sources
Launch Details

Launch Date

August 12, 2024

Launch Pad

LC39A

Launch Vehicle

Falcon 9

Orbital Elements

NORAD ID

60433

International Designator

2024-144J

Epoch

Sun, 19 Jul 2026 18:27:49 GMT

Apogee

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Perigee

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Inclination

53.16°

Right Ascension

322.75°

Eccentricity

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Argument of Perigee

88.59°

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-32183

Alternative Name

Starlink 32183

Type

Payload

Status

Operational

Owner

SPXS

Country

United States

Constellation

N/A

Related Satellites

Major Events

N/A

Latest TLEs
1 60433U 24144J   26200.76932403  .00000813  00000+0  35185-4 0  9992
2 60433  53.1631 322.7530 0000880  88.5918 271.5186 15.34393952109547

Source: Celestrak

Summary
The satellite identified by NORAD CAT ID 60433 and OBJECT ID 2024-144J is a Starlink V2M unit, part of the Starlink v2 Mini configuration series. Launched on August 12, 2024, from LC39A at AFETR using a Falcon 9 launch vehicle, this satellite was manufactured by SPXS for communication purposes. It has dimensions of 0.3 meters in length and 4.1 meters in diameter, with a span of 29 meters. The satellite weighs 700 kilograms dry and 730 kilograms at launch. Its equipment includes Ku/Ka/E-band payload and optical inter-satellite links, powered by solar arrays and batteries, and is equipped with Argon ion thrusters for propulsion. The shape of the spacecraft is described as a box with a pan configuration.

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 10-7-09

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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