STARLINK-30397 (57771)

COSPAR: 2023-134A | Alt Name: Starlink 30397

Image
STARLINK-30397 Satellite Image
Additional Sources
Launch Details

Launch Date

September 4, 2023

Launch Pad

LC39A

Launch Vehicle

Falcon 9

Orbital Elements

NORAD ID

57771

International Designator

2023-134A

Epoch

Sun, 19 Jul 2026 05:49:50 GMT

Apogee

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Perigee

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Inclination

43.00°

Right Ascension

171.77°

Eccentricity

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Argument of Perigee

258.78°

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-30397

Alternative Name

Starlink 30397

Type

Payload

Status

Operational

Owner

SPXS

Country

United States

Constellation

N/A

Related Satellites

Major Events

N/A

Latest TLEs
1 57771U 23134A   26200.24295073 -.00000464  00000+0 -73339-5 0  9997
2 57771  43.0046 171.7663 0000959 258.7831 101.2913 15.27570001159622

Source: Celestrak

Summary
The satellite named STARLINK-30397 (OBJECT_ID: 2023-134A) is a Starlink v2 Mini configuration built by SPXS for communication purposes. Launched on September 4, 2023, from the LC39A launch pad at AFETR using a Falcon 9 launch vehicle, it has a span of 29 meters and measures 0.3 meters in length with a diameter of 4.1 meters. The satellite weighs 730 kilograms at launch (with a dry mass of 700 kilograms) and is equipped with Ku/Ka/E-band payload, an optical inter-satellite link, and Argon ion thrusters for propulsion. It harnesses power through solar arrays and batteries and was manufactured by SPXS under the mission 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 6-12-01

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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