STARLINK-31180 (58732)

COSPAR: 2024-005E | Alt Name: Starlink 31180

Image
STARLINK-31180 Satellite Image
Additional Sources
Launch Details

Launch Date

January 7, 2024

Launch Pad

LC40

Launch Vehicle

Falcon 9

Orbital Elements

NORAD ID

58732

International Designator

2024-005E

Epoch

Sun, 19 Jul 2026 09:00:52 GMT

Apogee

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Perigee

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Inclination

43.00°

Right Ascension

196.04°

Eccentricity

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Argument of Perigee

275.11°

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-31180

Alternative Name

Starlink 31180

Type

Payload

Status

Operational

Owner

SPXS

Country

United States

Constellation

N/A

Related Satellites

Major Events

N/A

Latest TLEs
1 58732U 24005E   26200.37560409  .00000240  00000+0  18254-4 0  9999
2 58732  43.0040 196.0437 0001324 275.1102  84.9599 15.27575041140574

Source: Celestrak

Summary
The STARLINK-31180 satellite, also known as Starlink 31180, is a communication satellite belonging to SpaceX's Starlink v2 Mini constellation. It was launched on January 7, 2024, from Cape Canaveral Air Force Station's Launch Complex 40 aboard a Falcon 9 launch vehicle. The satellite has dimensions of 0.3 meters in length and 4.1 meters in diameter with an operational span of 29 meters. It weighs 730 kilograms at launch and 700 kilograms dry, featuring a configuration known as the Starlink V2M bus equipped with Argon ion thrusters for propulsion, solar arrays, and batteries for power supply. The satellite is designed for communication purposes and carries a Ku/Ka/E-band payload alongside an optical inter-satellite link system.

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 6-35-05

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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