STARLINK-32326 (61674)

COSPAR: 2024-193P | Alt Name: Starlink 32326

Image
STARLINK-32326 Satellite Image
Additional Sources
Launch Details

Launch Date

October 26, 2024

Launch Pad

LC40

Launch Vehicle

Falcon 9

Orbital Elements

NORAD ID

61674

International Designator

2024-193P

Epoch

Sun, 19 Jul 2026 09:49:50 GMT

Apogee

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Perigee

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Inclination

53.16°

Right Ascension

198.47°

Eccentricity

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Argument of Perigee

77.18°

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-32326

Alternative Name

Starlink 32326

Type

Payload

Status

Operational

Owner

SPXS

Country

United States

Constellation

N/A

Related Satellites

Major Events

N/A

Latest TLEs
1 61674U 24193P   26200.40961416  .00000531  00000+0  28883-4 0  9995
2 61674  53.1586 198.4652 0001124  77.1773 282.9354 15.31704821 96706

Source: Celestrak

Summary
The STARLINK-32326 satellite, also known as Starlink 32326, is a communication satellite belonging to the Starlink v2 Mini configuration under SpaceX (SPXS). Launched on October 26, 2024, from LC40 at AFETR using a 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 is equipped with a Ku/Ka/E-band payload and an optical inter-satellite link for communication purposes. It features solar arrays and batteries for power generation and utilizes Argon ion thrusters as its propulsion system. The dry mass of the satellite is 700 kg, with a launch mass of 730 kg.

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 10-8-14

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

Map
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