STARLINK-31319 (59457)

COSPAR: 2024-068C | Alt Name: Starlink 31319

Image
STARLINK-31319 Satellite Image
Additional Sources
Launch Details

Launch Date

April 10, 2024

Launch Pad

LC40

Launch Vehicle

Falcon 9

Orbital Elements

NORAD ID

59457

International Designator

2024-068C

Epoch

Mon, 20 Jul 2026 03:51:31 GMT

Apogee

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Perigee

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Inclination

43.00°

Right Ascension

2.83°

Eccentricity

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Argument of Perigee

269.59°

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-31319

Alternative Name

Starlink 31319

Type

Payload

Status

Operational

Owner

SPXS

Country

United States

Constellation

N/A

Related Satellites

Major Events

N/A

Latest TLEs
1 59457U 24068C   26201.16078392 -.00000220  00000+0  15311-5 0  9997
2 59457  43.0026   2.8322 0001386 269.5885  90.4808 15.27580448128829

Source: Celestrak

Summary
STARLINK-31319 is a communication satellite under the Starlink v2 Mini configuration, launched on April 10, 2024, from Launch Complex 40 at the Cape Canaveral Space Force Station 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, featuring solar arrays and batteries for power supply. It is equipped with a Ku/Ka/E-band payload and an optical inter-satellite link, and uses Argon ion thrusters as its motor system. The satellite's dry mass is 700 kilograms while its launch mass was 730 kilograms. Manufactured by SpaceX (SPXS), it is part of the Starlink Group 6-48-03 constellation for communication purposes.

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 6-48-03

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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