STARLINK-30477 (57912)

COSPAR: 2023-146X | Alt Name: Starlink 30477

Image
STARLINK-30477 Satellite Image
Additional Sources
Launch Details

Launch Date

September 20, 2023

Launch Pad

LC40

Launch Vehicle

Falcon 9

Orbital Elements

NORAD ID

57912

International Designator

2023-146X

Epoch

Sun, 19 Jul 2026 06:42:41 GMT

Apogee

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Perigee

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Inclination

43.00°

Right Ascension

287.44°

Eccentricity

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Argument of Perigee

273.10°

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-30477

Alternative Name

Starlink 30477

Type

Payload

Status

Operational

Owner

SPXS

Country

United States

Constellation

N/A

Related Satellites

Major Events

N/A

Latest TLEs
1 57912U 23146X   26200.27964391  .00000020  00000+0  10271-4 0  9997
2 57912  43.0026 287.4368 0001437 273.1024  86.9663 15.27578848157223

Source: Celestrak

Summary
The Starlink-30477 satellite, also known as Starlink 30477, is a communications spacecraft belonging to the Starlink v2 Mini configuration under SpaceX's fleet. Launched on September 20, 2023, from LC40 at AFETR using a Falcon 9 launch vehicle, this satellite has a dry mass of 700 kilograms and a launch mass of 730 kilograms. It measures 0.3 meters in length with a diameter of 4.1 meters and a span of 29 meters. Equipped with Ku/Ka/E-band payload and an optical inter-satellite link, the satellite is powered by solar arrays and batteries. Its propulsion system includes Argon ion thrusters for orbital adjustments. The mission purpose is to enhance communication capabilities as part of SpaceX's Starlink Group 6-17-22 constellation.

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 6-17-22

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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