STARLINK-32327 (61641)

COSPAR: 2024-191W | Alt Name: Starlink 32327

Image
STARLINK-32327 Satellite Image
Additional Sources
Launch Details

Launch Date

October 23, 2024

Launch Pad

LC40

Launch Vehicle

Falcon 9

Orbital Elements

NORAD ID

61641

International Designator

2024-191W

Epoch

Mon, 20 Jul 2026 04:43:07 GMT

Apogee

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Perigee

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Inclination

43.00°

Right Ascension

126.00°

Eccentricity

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Argument of Perigee

266.52°

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
Basic Satellite Info

Name

STARLINK-32327

Alternative Name

Starlink 32327

Type

Payload

Status

Operational

Owner

SPXS

Country

United States

Constellation

N/A

Related Satellites

Major Events

N/A

Latest TLEs
1 61641U 24191W   26201.19660883  .00000208  00000+0  17066-4 0  9990
2 61641  43.0019 125.9957 0001213 266.5160  93.5553 15.27583225 97802

Source: Celestrak

Summary
The satellite identified by NORAD_CAT_ID 61641 and OBJECT_ID 2024-191W is a Starlink V2M spacecraft, part of the Starlink v2 Mini configuration. Launched on October 23, 2024, from LC40 at AFETR using a Falcon 9 launch vehicle, this satellite has a dry mass of 700 kg and a launch mass of 730 kg. It measures 0.3 meters in length with a diameter of 4.1 meters and spans 29 meters. The satellite is equipped with a Ku/Ka/E-band payload, an optical inter-satellite link, Argon ion thrusters for propulsion, solar arrays, and batteries for power generation. Its primary mission is communication as part of the Starlink Group 6-61-21 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 6-61-21

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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