STARLINK-30375 (57732)

COSPAR: 2023-131A | Alt Name: Starlink 30375

Image
STARLINK-30375 Satellite Image
Additional Sources
Launch Details

Launch Date

September 1, 2023

Launch Pad

LC40

Launch Vehicle

Falcon 9

Orbital Elements

NORAD ID

57732

International Designator

2023-131A

Epoch

Sun, 19 Jul 2026 20:29:26 GMT

Apogee

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Perigee

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Inclination

43.01°

Right Ascension

131.22°

Eccentricity

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Argument of Perigee

262.95°

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-30375

Alternative Name

Starlink 30375

Type

Payload

Status

Operational

Owner

SPXS

Country

United States

Constellation

N/A

Related Satellites

Major Events

N/A

Latest TLEs
1 57732U 23131A   26200.85378235 -.00000250  00000+0  42792-6 0  9992
2 57732  43.0052 131.2155 0001296 262.9486  97.1218 15.27576290160316

Source: Celestrak

Summary
The STARLINK-30375 satellite, also known as Starlink 30375, is a communication satellite manufactured by SPXS and part of the Starlink v2 Mini configuration. It was launched on September 1, 2023, from LC40 at AFETR using a Falcon 9 launch vehicle. The satellite has dimensions of 0.3 meters in length, a diameter of 4.1 meters, and a span of 29 meters. Its dry mass is 700 kg and it weighs 730 kg at launch. It carries a Ku/Ka/E-band payload with an optical inter-satellite link and uses solar arrays and batteries for power. The satellite's propulsion system includes Argon ion thrusters, and its mission is to provide communication services.

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 6-13-01

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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