STARLINK-32547 (61919)

COSPAR: 2024-207H | Alt Name: Starlink 32547

Image
STARLINK-32547 Satellite Image
Additional Sources
Launch Details

Launch Date

November 11, 2024

Launch Pad

LC40

Launch Vehicle

Falcon 9

Orbital Elements

NORAD ID

61919

International Designator

2024-207H

Epoch

Sun, 19 Jul 2026 21:08:11 GMT

Apogee

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Perigee

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Inclination

43.00°

Right Ascension

254.80°

Eccentricity

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Argument of Perigee

265.78°

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-32547

Alternative Name

Starlink 32547

Type

Payload

Status

Operational

Owner

SPXS

Country

United States

Constellation

N/A

Related Satellites

Major Events

N/A

Latest TLEs
1 61919U 24207H   26200.88069192  .00003854  00000+0  14949-3 0  9993
2 61919  43.0030 254.7989 0002251 265.7803  94.2791 15.27585040 94937

Source: Celestrak

Summary
The STARLINK-32547 satellite, also known as Starlink 32547, is a communication satellite manufactured by SPXS and operated under the Starlink Group 6-69-08 mission. Launched on November 11, 2024, from LC40 at AFETR using a Falcon 9 launch vehicle, it has a configuration known as Starlink v2 Mini with dimensions including a length of 0.3 meters, diameter of 4.1 meters, and a span of 29 meters. The satellite carries a Ku/Ka/E-band payload along with an optical inter-satellite link for communication purposes and is equipped with Argon ion thrusters for propulsion. It features solar arrays and batteries for power supply and has a dry mass of 700 kilograms and a launch mass of 730 kilograms.

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 6-69-08

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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