STARLINK-32395 (61679)

COSPAR: 2024-193U | Alt Name: Starlink 32395

Image

Additional Sources

Launch Details

Launch Date

October 26, 2024

Launch Site

Cape Canaveral Space Force Station

Launch Pad

LC40

Launch Vehicle

Falcon 9

Orbital Elements

NORAD ID

61679

International Designator

2024-193U

Epoch

Sun, 19 Jul 2026 09:01:26 GMT

Apogee

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Perigee

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Inclination

53.16°

Right Ascension

199.67°

Eccentricity

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Argument of Perigee

83.91°

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

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Starlink V2M bus SpaceX Starlink constellation United States satellites Payloads

Basic Satellite Info

Name

STARLINK-32395

Alternative Name

Starlink 32395

Type

Payload

Status

Operational

Owner

SPXS

Country

United States

Constellation

N/A

Related Satellites

Major Events

N/A

Latest TLEs

1 61679U 24193U   26200.37599582 -.00000352  00000+0  23495-6 0  9995

2 61679  53.1588 199.6706 0001283  83.9148 276.1999 15.30187791 96680

Source: Celestrak

Summary

The satellite named STARLINK-32395 (OBJECT_ID: 2024-193U) is a Starlink V2M configuration operated by SpaceX (SPXS). It was launched on October 26, 2024, from Cape Canaveral Air Force Station's Launch Complex 40 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. It weighs 700 kilograms dry with a total launch mass of 730 kilograms. Equipped with a Ku/Ka/E-band payload and an optical inter-satellite link, it utilizes solar arrays and batteries for power. The satellite is configured to perform communication tasks using Argon ion thrusters as its propulsion system.

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

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 10-8-19

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

Map

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