STARLINK-32203 (60331)

COSPAR: 2024-136C | Alt Name: Starlink 32203

Image
STARLINK-32203 Satellite Image
Additional Sources
Launch Details

Launch Date

August 2, 2024

Launch Pad

LC39A

Launch Vehicle

Falcon 9

Orbital Elements

NORAD ID

60331

International Designator

2024-136C

Epoch

Mon, 20 Jul 2026 02:59:49 GMT

Apogee

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Perigee

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Inclination

53.16°

Right Ascension

168.97°

Eccentricity

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Argument of Perigee

88.17°

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-32203

Alternative Name

Starlink 32203

Type

Payload

Status

Operational

Owner

SPXS

Country

United States

Constellation

N/A

Related Satellites

Major Events

N/A

Latest TLEs
1 60331U 24136C   26201.12487788  .00000579  00000+0  28274-4 0  9992
2 60331  53.1594 168.9721 0001401  88.1660 271.9503 15.34392791110105

Source: Celestrak

Summary
The STARLINK-32203 satellite, also known as Starlink 32203, is a communication satellite designed under the Starlink v2 Mini configuration and manufactured by SPXS (SpaceX). It was launched on August 2, 2024, from Launch Complex 39A at Kennedy Space Center using a Falcon 9 launch vehicle. The satellite has dimensions of 0.3 meters in length, 4.1 meters in diameter, and spans 29 meters when fully deployed. At launch, it weighed 730 kg with a dry mass of 700 kg. It is equipped with Ku/Ka/E-band payload capabilities and an optical inter-satellite link. Power for the satellite is provided by solar arrays and batteries. The propulsion system consists of Argon ion thrusters.

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 10-6-03

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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