STARLINK-32365 (61625)

COSPAR: 2024-191E | Alt Name: Starlink 32365

Image

Additional Sources

Launch Details

Launch Date

October 23, 2024

Launch Site

Cape Canaveral Space Force Station

Launch Pad

LC40

Launch Vehicle

Falcon 9

Orbital Elements

NORAD ID

61625

International Designator

2024-191E

Epoch

Mon, 20 Jul 2026 04:37:34 GMT

Apogee

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Perigee

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Inclination

43.00°

Right Ascension

125.97°

Eccentricity

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Argument of Perigee

259.18°

Period

94.27 min

Mean Motion

15.28 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-32365

Alternative Name

Starlink 32365

Type

Payload

Status

Operational

Owner

SPXS

Country

United States

Constellation

N/A

Related Satellites

Major Events

N/A

Latest TLEs

1 61625U 24191E   26201.19276088  .00000001  00000+0  95747-5 0  9996

2 61625  43.0029 125.9709 0001236 259.1775 100.8938 15.27579082 97800

Source: Celestrak

Summary

The STARLINK-32365 satellite, also known as Starlink 32365, is a communication satellite belonging to the Starlink v2 Mini configuration and was launched on October 23, 2024, from LC40 at AFETR using a Falcon 9 launch vehicle. This spacecraft has a length of 0.3 meters, a diameter of 4.1 meters, and a span of 29 meters, with a dry mass of 700 kg and a launch mass of 730 kg. It is equipped with Ku/Ka/E-band payload and optical inter-satellite link equipment, powered by solar arrays and batteries, and uses Argon ion thrusters for propulsion. The satellite's purpose is communication, and it was manufactured by SPXS and owned by the same entity under the Starlink Group 6-61-05 payload.

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 6-61-05

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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