STARLINK-32534 (62175)

COSPAR: 2024-225N | Alt Name: Starlink 32534

Image
STARLINK-32534 Satellite Image
Additional Sources
Launch Details

Launch Date

November 30, 2024

Launch Site

AFWTR

Launch Pad

SLC4E

Launch Vehicle

Falcon 9

Orbital Elements

NORAD ID

62175

International Designator

2024-225N

Epoch

Sun, 19 Jul 2026 08:34:07 GMT

Apogee

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Perigee

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Inclination

70.00°

Right Ascension

192.63°

Eccentricity

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Argument of Perigee

265.49°

Period

96.11 min

Mean Motion

14.98 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-32534

Alternative Name

Starlink 32534

Type

Payload

Status

Operational

Owner

SPXS

Country

United States

Constellation

N/A

Related Satellites

Major Events

N/A

Latest TLEs
1 62175U 24225N   26200.35702816  .00001512  00000+0  13444-3 0  9995
2 62175  70.0001 192.6283 0003809 265.4884  94.5840 14.98334156 89594

Source: Celestrak

Summary
The Starlink-32534 satellite, also known as Starlink 32534, is a communication satellite built by SpaceX (SPXS) and launched on November 30, 2024, from AFWTR SLC4E using the Falcon 9 launch vehicle. With a configuration of Starlink v2 Mini, it has dimensions of 0.3 meters in length, 4.1 meters in diameter, and a span of 29 meters. The satellite's dry mass is 700 kg with a total launch mass of 730 kg. It is equipped with Ku/Ka/E-band payload and an optical inter-satellite link for data transmission, powered by solar arrays and batteries. The propulsion system uses Argon ion thrusters for orbital maneuvers. Its purpose is to provide communication services as part of the Starlink Group N-01-11 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 N-01-11

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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