STARLINK-31537 (59365)

COSPAR: 2024-060T | Alt Name: Starlink 31537

Image
STARLINK-31537 Satellite Image
Additional Sources
Launch Details

Launch Date

March 31, 2024

Launch Pad

LC40

Launch Vehicle

Falcon 9

Orbital Elements

NORAD ID

59365

International Designator

2024-060T

Epoch

Sun, 19 Jul 2026 19:08:34 GMT

Apogee

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Perigee

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Inclination

43.00°

Right Ascension

234.07°

Eccentricity

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Argument of Perigee

275.94°

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-31537

Alternative Name

Starlink 31537

Type

Payload

Status

Operational

Owner

SPXS

Country

United States

Constellation

N/A

Related Satellites

Major Events

N/A

Latest TLEs
1 59365U 24060T   26200.79762083  .00000272  00000+0  19417-4 0  9998
2 59365  43.0012 234.0686 0001476 275.9422  84.1262 15.27578785130268

Source: Celestrak

Summary
STARLINK-31537 is a Starlink v2 Mini satellite, part of the Starlink Group 6-45-18 constellation, launched on March 31, 2024, from LC40 at AFETR using a Falcon 9 launch vehicle. The spacecraft measures 0.3 meters in length with a diameter of 4.1 meters and a span of 29 meters. It has a dry mass of 700 kilograms and a launch mass of 730 kilograms. Equipped with Ku/Ka/E-band payload, optical inter-satellite link, and Argon ion thrusters for propulsion, the satellite is powered by solar arrays and batteries. The purpose of this communication satellite is to provide internet services as part of SpaceX's Starlink constellation. The spacecraft has a box shape with an additional pan structure.

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 6-45-18

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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