STARLINK-30147 (57511)

COSPAR: 2023-113S | Alt Name: Starlink 30147

Image
STARLINK-30147 Satellite Image
Additional Sources
Launch Details

Launch Date

August 7, 2023

Launch Pad

LC40

Launch Vehicle

Falcon 9

Orbital Elements

NORAD ID

57511

International Designator

2023-113S

Epoch

Sun, 19 Jul 2026 19:24:27 GMT

Apogee

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Perigee

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Inclination

43.01°

Right Ascension

349.72°

Eccentricity

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Argument of Perigee

257.70°

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-30147

Alternative Name

Starlink 30147

Type

Payload

Status

Operational

Owner

SPXS

Country

United States

Constellation

N/A

Related Satellites

Major Events

N/A

Latest TLEs
1 57511U 23113S   26200.80865381  .00000460  00000+0  26268-4 0  9995
2 57511  43.0058 349.7157 0001541 257.7041 102.3638 15.27570531163889

Source: Celestrak

Summary
The Starlink-30147 satellite, also known as STARLINK-30147 or Starlink 30147, is a part of the Starlink v2 Mini configuration and belongs to SpaceX (SPXS). It was launched on August 7, 2023, from the Cape Canaveral Space Force Station Launch Complex 40 using a Falcon 9 launch vehicle. The satellite has dimensions of 0.3 meters in length, 4.1 meters in diameter, and a span of 29 meters. It weighs 730 kg at launch with a dry mass of 700 kg. Equipped with Ku/Ka/E-band payload and optical inter-satellite link for communication purposes, it utilizes solar arrays and batteries for power supply and Argon ion thrusters as its motor system. Its primary mission is to provide global 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 6-8-17

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

Map
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