STARLINK-32020 (60201)

COSPAR: 2024-124U | Alt Name: Starlink 32020

Image
STARLINK-32020 Satellite Image
Additional Sources
Launch Details

Launch Date

July 3, 2024

Launch Pad

LC40

Launch Vehicle

Falcon 9

Orbital Elements

NORAD ID

60201

International Designator

2024-124U

Epoch

Sun, 19 Jul 2026 23:57:20 GMT

Apogee

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Perigee

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Inclination

53.16°

Right Ascension

67.16°

Eccentricity

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Argument of Perigee

89.19°

Period

94.01 min

Mean Motion

15.32 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-32020

Alternative Name

Starlink 32020

Type

Payload

Status

Operational

Owner

SPXS

Country

United States

Constellation

N/A

Related Satellites

Major Events

N/A

Latest TLEs
1 60201U 24124U   26200.99815457 -.00000667  00000+0 -97201-5 0  9994
2 60201  53.1611  67.1571 0001435  89.1892 270.9274 15.31708070114565

Source: Celestrak

Summary
The STARLINK-32020 satellite, also known as Starlink 32020, is a communication satellite developed by SPXS and launched on July 3, 2024, from the Air Force Eastern Test Range (AFETR) using a Falcon 9 launch vehicle. It has a configuration of Starlink v2 Mini with dimensions including a length of 0.3 meters, diameter of 4.1 meters, and span of 29 meters. The satellite's dry mass is 700 kg, and it weighs 730 kg at launch. Equipped with Ku/Ka/E-band payload and an optical inter-satellite link, the STARLINK-32020 utilizes Argon ion thrusters for propulsion and solar arrays combined with batteries for power. Its primary purpose is to provide communication services as part of the Starlink Group 8-9-19 constellation.

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 8-9-19

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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