STARLINK-31519 (59546)

COSPAR: 2024-074N | Alt Name: Starlink 31519

Image
STARLINK-31519 Satellite Image
Additional Sources
Launch Details

Launch Date

April 18, 2024

Launch Pad

LC40

Launch Vehicle

Falcon 9

Orbital Elements

NORAD ID

59546

International Designator

2024-074N

Epoch

Sun, 19 Jul 2026 16:09:05 GMT

Apogee

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Perigee

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Inclination

43.00°

Right Ascension

317.79°

Eccentricity

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Argument of Perigee

261.59°

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-31519

Alternative Name

Starlink 31519

Type

Payload

Status

Operational

Owner

SPXS

Country

United States

Constellation

N/A

Related Satellites

Major Events

N/A

Latest TLEs
1 59546U 24074N   26200.67298417  .00000819  00000+0  39276-4 0  9998
2 59546  43.0019 317.7946 0001315 261.5854  98.4849 15.27581587126208

Source: Celestrak

Summary
STARLINK-31519 is a communication satellite belonging to the Starlink v2 Mini configuration, categorized under NORAD CAT ID 59546 and OBJECT ID 2024-074N. Launched on April 18, 2024, from AFETR's LC40 pad using a Falcon 9 launch vehicle, it was manufactured by SPXS in the United States. The satellite measures 0.3 meters in length and has a diameter of 4.1 meters with a span of 29 meters. It carries a Ku/Ka/E-band payload and an optical inter-satellite link, powered by solar arrays and batteries. Equipped with Argon ion thrusters for propulsion, the satellite weighs 700 kilograms dry and had a launch mass of 730 kilograms. Its mission is to facilitate communication services as part of the Starlink Group 6-52-13 constellation, owned by 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 6-52-13

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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