STARLINK-30134 (56830)

COSPAR: 2023-079H | Alt Name: Starlink 30134
DECAYED

Image
STARLINK-30134 Satellite Image
Additional Sources
Launch Details

Launch Date

June 4, 2023

Launch Pad

LC40

Launch Vehicle

Falcon 9

Orbital Elements

NORAD ID

56830

International Designator

2023-079H

Decay Date

7/18/2023

Basic Satellite Info

Name

STARLINK-30134

Alternative Name

Starlink 30134

Type

Payload

Status

Decayed

Owner

SPXS

Country

United States

Constellation

N/A

Related Satellites

Major Events

N/A

Summary
The satellite identified by NORAD_CAT_ID 56830 and OBJECT_ID 2023-079H is named STARLINK-30134 or Starlink 30134, part of the Starlink v2 Mini configuration series manufactured by SPXS (SpaceX). It was launched on June 4, 2023, from LC40 at AFETR (Cape Canaveral Space Force Station) using a Falcon 9 launch vehicle. The satellite's dimensions are 0.3 meters in length and has a diameter of 4.1 meters with a span of 29 meters. It weighs 730 kilograms at launch, reducing to a dry mass of 700 kilograms post-launch operations. Equipped with Ku/Ka/E-band payload and an optical inter-satellite link for communication purposes, it also features solar arrays and batteries for power supply, along with Argon ion thrusters as its propulsion system. The satellite's shape is described as box-shaped with a pan, and its primary 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 6-4-08

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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