STARLINK-31818 (59741)

COSPAR: 2024-090M | Alt Name: Starlink 31818

Image
STARLINK-31818 Satellite Image
Additional Sources
Launch Details

Launch Date

May 13, 2024

Launch Pad

LC40

Launch Vehicle

Falcon 9

Orbital Elements

NORAD ID

59741

International Designator

2024-090M

Epoch

Sun, 19 Jul 2026 05:18:34 GMT

Apogee

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Perigee

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Inclination

43.00°

Right Ascension

160.89°

Eccentricity

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Argument of Perigee

267.67°

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-31818

Alternative Name

Starlink 31818

Type

Payload

Status

Operational

Owner

SPXS

Country

United States

Constellation

N/A

Related Satellites

Major Events

N/A

Latest TLEs
1 59741U 24090M   26200.22123168 -.00000182  00000+0  29233-5 0  9991
2 59741  43.0041 160.8892 0001542 267.6715  92.3960 15.27564967123557

Source: Celestrak

Summary
The Starlink-31818 satellite, designated OBJECT_ID 2024-090M, is a member of the Starlink v2 Mini configuration and was launched on May 13, 2024, from Cape Canaveral Space Force Station Launch Complex 40 using a Falcon 9 launch vehicle. The spacecraft measures 0.3 meters in length with a diameter of 4.1 meters and has a span of 29 meters due to its deployable components. It has a dry mass of 700 kilograms and was launched with a total mass of 730 kilograms. Equipped with a Ku/Ka/E-band payload and an optical inter-satellite link, the satellite uses Argon ion thrusters for propulsion and solar arrays along with batteries to power its systems. The mission purpose is communication, owned and operated by SpaceX (SPXS).

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 6-58-12

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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