STARLINK-31592 (59467)

COSPAR: 2024-068N | Alt Name: Starlink 31592

Image
STARLINK-31592 Satellite Image
Additional Sources
Launch Details

Launch Date

April 10, 2024

Launch Pad

LC40

Launch Vehicle

Falcon 9

Orbital Elements

NORAD ID

59467

International Designator

2024-068N

Epoch

Sun, 19 Jul 2026 19:06:35 GMT

Apogee

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Perigee

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Inclination

43.01°

Right Ascension

8.71°

Eccentricity

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Argument of Perigee

260.80°

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-31592

Alternative Name

Starlink 31592

Type

Payload

Status

Operational

Owner

SPXS

Country

United States

Constellation

N/A

Related Satellites

Major Events

N/A

Latest TLEs
1 59467U 24068N   26200.79624875  .00001102  00000+0  49579-4 0  9990
2 59467  43.0050   8.7138 0001488 260.7988  99.2696 15.27584066128728

Source: Celestrak

Summary
STARLINK-31592 is a Starlink v2 Mini satellite identified by NORAD catalog ID 59467 and object ID 2024-068N, manufactured by SPXS in the US. Launched on April 10, 2024, from LC40 at AFETR using a Falcon 9 launch vehicle, it has dimensions of 0.3 meters in length, 4.1 meters in diameter, and a span of 29 meters. The satellite weighs 700 kilograms dry with a total launch mass of 730 kilograms. It is equipped with Ku/Ka/E-band payload capabilities and an optical inter-satellite link for communication purposes. Power is supplied by solar arrays and batteries. Its propulsion system includes Argon ion thrusters, and it was stabilized on April 10, 2024, at 06:45:34 UTC. The satellite's shape resembles a box with a pan configuration.

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 6-48-13

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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