STARLINK-31819 (59738)

COSPAR: 2024-090J | Alt Name: Starlink 31819

Image
STARLINK-31819 Satellite Image
Additional Sources
Launch Details

Launch Date

May 13, 2024

Launch Pad

LC40

Launch Vehicle

Falcon 9

Orbital Elements

NORAD ID

59738

International Designator

2024-090J

Epoch

Sun, 19 Jul 2026 22:12:04 GMT

Apogee

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Perigee

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Inclination

43.00°

Right Ascension

156.71°

Eccentricity

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Argument of Perigee

264.57°

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-31819

Alternative Name

Starlink 31819

Type

Payload

Status

Operational

Owner

SPXS

Country

United States

Constellation

N/A

Related Satellites

Major Events

N/A

Latest TLEs
1 59738U 24090J   26200.92504638 -.00000047  00000+0  78066-5 0  9997
2 59738  43.0024 156.7136 0000851 264.5701  95.5054 15.27576661123667

Source: Celestrak

Summary
The satellite STARLINK-31819 (OBJECT_ID: 2024-090J) is a Starlink v2 Mini configuration manufactured by SPXS and owned by the same entity. It was launched on May 13, 2024, from Cape Canaveral Space Force Station's Launch Complex 40 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. It weighs 730 kg at launch and has a dry mass of 700 kg. Equipped with Ku/Ka/E-band payload and an optical inter-satellite link, it utilizes Argon ion thrusters for propulsion and solar arrays along with batteries for power generation. The satellite's mission is communication.

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 6-58-09

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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