STARLINK-32204 (60584)

COSPAR: 2024-150B | Alt Name: Starlink 32204

Image
STARLINK-32204 Satellite Image
Additional Sources
Launch Details

Launch Date

August 20, 2024

Launch Pad

LC40

Launch Vehicle

Falcon 9

Orbital Elements

NORAD ID

60584

International Designator

2024-150B

Epoch

Sun, 19 Jul 2026 19:36:09 GMT

Apogee

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Perigee

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Inclination

53.16°

Right Ascension

50.97°

Eccentricity

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Argument of Perigee

87.93°

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-32204

Alternative Name

Starlink 32204

Type

Payload

Status

Operational

Owner

SPXS

Country

United States

Constellation

N/A

Related Satellites

Major Events

N/A

Latest TLEs
1 60584U 24150B   26200.81677580 -.00000605  00000+0 -67715-5 0  9990
2 60584  53.1596  50.9719 0001331  87.9285 272.1870 15.34397229108306

Source: Celestrak

Summary
The Starlink V2M satellite, designated STARLINK-32204 or Starlink 32204, is a communication satellite manufactured by SpaceX (SPXS) and launched on August 20, 2024, from Cape Canaveral Air Force Station's Launch Complex 40 using the Falcon 9 launch vehicle. It has dimensions of 0.3 meters in length, 4.1 meters in diameter, and a span of 29 meters. The satellite weighs 700 kilograms dry and 730 kilograms at launch. Equipped with Ku/Ka/E-band payload and an optical inter-satellite link, it uses Argon ion thrusters for propulsion and solar arrays along with batteries for power. Its shape is described as a box with a pan configuration. The satellite operates in the Starlink Group 10-5-02 constellation and was launched to provide communication services.

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 10-5-02

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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