STARLINK-31551 (59191)

COSPAR: 2024-045P | Alt Name: Starlink 31551

Image

Additional Sources

Launch Details

Launch Date

March 10, 2024

Launch Site

Cape Canaveral Space Force Station

Launch Pad

LC40

Launch Vehicle

Falcon 9

Orbital Elements

NORAD ID

59191

International Designator

2024-045P

Epoch

Sun, 19 Jul 2026 22:54:49 GMT

Apogee

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Perigee

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Inclination

43.00°

Right Ascension

61.80°

Eccentricity

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Argument of Perigee

263.09°

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

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Starlink V2M bus SpaceX Starlink constellation United States satellites Payloads

Basic Satellite Info

Name

STARLINK-31551

Alternative Name

Starlink 31551

Type

Payload

Status

Operational

Owner

SPXS

Country

United States

Constellation

N/A

Related Satellites

Major Events

N/A

Latest TLEs

1 59191U 24045P   26200.95474242  .00000203  00000+0  16885-4 0  9993

2 59191  43.0027  61.7982 0001338 263.0913  96.9786 15.27580058133435

Source: Celestrak

Summary

The satellite named STARLINK-31551 (OBJECT_ID: 2024-045P) is a Starlink v2 Mini communication satellite manufactured by SPXS and launched on March 10, 2024, from Cape Canaveral Air Force Station's LC40 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 kilograms at launch with a dry mass of 700 kilograms. Equipped with Ku/Ka/E-band payload and optical inter-satellite links for communication purposes, it uses solar arrays and batteries for power. The satellite also features Argon ion thrusters as its motor 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

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 6-43-14

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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Latitude

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