STARLINK-30307 (57747)

COSPAR: 2023-131R | Alt Name: Starlink 30307

Image
STARLINK-30307 Satellite Image
Additional Sources
Launch Details

Launch Date

September 1, 2023

Launch Pad

LC40

Launch Vehicle

Falcon 9

Orbital Elements

NORAD ID

57747

International Designator

2023-131R

Epoch

Sun, 19 Jul 2026 19:55:34 GMT

Apogee

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Perigee

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Inclination

43.00°

Right Ascension

146.36°

Eccentricity

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Argument of Perigee

267.26°

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-30307

Alternative Name

Starlink 30307

Type

Payload

Status

Operational

Owner

SPXS

Country

United States

Constellation

N/A

Related Satellites

Major Events

N/A

Latest TLEs
1 57747U 23131R   26200.83025544  .00000796  00000+0  38436-4 0  9990
2 57747  43.0033 146.3616 0000857 267.2645  92.8108 15.27579160160125

Source: Celestrak

Summary
STARLINK-30307 is a Starlink V2M satellite configured in the Starlink v2 Mini design, launched by SpaceX on September 1, 2023, from LC40 at AFETR using a Falcon 9 launch vehicle. The satellite has dimensions of 0.3 meters in length and 4.1 meters in diameter with a span of 29 meters. It weighs 730 kilograms at launch and 700 kilograms dry mass. Equipped with a Ku/Ka/E-band payload and an optical inter-satellite link, it is powered by solar arrays and batteries. The satellite uses Argon ion thrusters for propulsion and is designed for communication purposes as part of the Starlink Group 6-13-16 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 6-13-16

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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