STARLINK-32375 (61070)

COSPAR: 2024-164W | Alt Name: Starlink 32375

Image
STARLINK-32375 Satellite Image
Additional Sources
Launch Details

Launch Date

September 13, 2024

Launch Site

AFWTR

Launch Pad

SLC4E

Launch Vehicle

Falcon 9

Orbital Elements

NORAD ID

61070

International Designator

2024-164W

Epoch

Mon, 20 Jul 2026 03:16:40 GMT

Apogee

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Perigee

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Inclination

53.16°

Right Ascension

196.06°

Eccentricity

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Argument of Perigee

62.49°

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
Basic Satellite Info

Name

STARLINK-32375

Alternative Name

Starlink 32375

Type

Payload

Status

Operational

Owner

SPXS

Country

United States

Constellation

N/A

Related Satellites

Major Events

N/A

Latest TLEs
1 61070U 24164W   26201.13658051  .00000915  00000+0  43019-4 0  9996
2 61070  53.1592 196.0639 0001380  62.4865 297.6276 15.30196680103752

Source: Celestrak

Summary
The Starlink-32375 satellite, also known as STARLINK-32375, is a communication satellite belonging to the Starlink v2 Mini configuration and launched on September 13, 2024, from AFWTR SLC4E using a Falcon 9 launch vehicle. With a length of 0.3 meters, diameter of 4.1 meters, and span of 29 meters, it has a dry mass of 700 kg and was launched with a mass of 730 kg. Equipped with Ku/Ka/E-band payload and an optical inter-satellite link, the satellite uses solar arrays and batteries for power supply and argon ion thrusters for propulsion. The mission is to provide communication services as part of the Starlink Group 9-6-21 constellation managed by SPXS (SpaceX).

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 9-6-21

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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