STARLINK-32039 (60604)

COSPAR: 2024-150X | Alt Name: Starlink 32039

Image
STARLINK-32039 Satellite Image
Additional Sources
Launch Details

Launch Date

August 20, 2024

Launch Pad

LC40

Launch Vehicle

Falcon 9

Orbital Elements

NORAD ID

60604

International Designator

2024-150X

Epoch

Mon, 20 Jul 2026 06:50:43 GMT

Apogee

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Perigee

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Inclination

53.16°

Right Ascension

53.88°

Eccentricity

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Argument of Perigee

98.66°

Period

94.11 min

Mean Motion

15.30 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-32039

Alternative Name

Starlink 32039

Type

Payload

Status

Operational

Owner

SPXS

Country

United States

Constellation

N/A

Related Satellites

Major Events

N/A

Latest TLEs
1 60604U 24150X   26201.28522470  .00001353  00000+0  57815-4 0  9990
2 60604  53.1599  53.8828 0001327  98.6632 261.4519 15.30198178108304

Source: Celestrak

Summary
STARLINK-32039, also known as Starlink 32039, is a communication satellite part of the Starlink v2 Mini configuration and belongs to SpaceX (SPXS). Launched on August 20, 2024, from LC40 at AFETR using a Falcon 9 launch vehicle, it measures 0.3 meters in length with a diameter of 4.1 meters and a span of 29 meters. The satellite has a dry mass of 700 kilograms and a launch mass of 730 kilograms. It is equipped with a Ku/Ka/E-band payload and an optical inter-satellite link, powered by solar arrays and batteries. Its propulsion system includes Argon ion thrusters for maneuvering in orbit.

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 10-5-22

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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