STARLINK-31940 (59873)

COSPAR: 2024-098R | Alt Name: Starlink 31940

Image
STARLINK-31940 Satellite Image
Additional Sources
Launch Details

Launch Date

May 24, 2024

Launch Pad

LC39A

Launch Vehicle

Falcon 9

Orbital Elements

NORAD ID

59873

International Designator

2024-098R

Epoch

Sun, 19 Jul 2026 12:07:21 GMT

Apogee

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Perigee

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Inclination

43.00°

Right Ascension

245.96°

Eccentricity

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Argument of Perigee

270.83°

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-31940

Alternative Name

Starlink 31940

Type

Payload

Status

Operational

Owner

SPXS

Country

United States

Constellation

N/A

Related Satellites

Major Events

N/A

Latest TLEs
1 59873U 24098R   26200.50511227 -.00000119  00000+0  52020-5 0  9993
2 59873  43.0020 245.9554 0001175 270.8342  89.2375 15.27574779122099

Source: Celestrak

Summary
The satellite named STARLINK-31940 (OBJECT_ID: 2024-098R) is a Starlink v2 Mini communication satellite manufactured by SPXS and launched on May 24, 2024, from LC39A at AFETR using a Falcon 9 launch vehicle. It has dimensions of 0.3 meters in length, 4.1 meters in diameter, and spans 29 meters with its equipment including Ku/Ka/E-band payload and an optical inter-satellite link. The satellite weighs 700 kilograms dry and 730 kilograms at launch. Its power source consists of solar arrays and batteries, and it is equipped with Argon ion thrusters for propulsion. The satellite's shape is described as a box with a pan configuration and is part of the Starlink Group 6-63-16 payload mission focused on 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 6-63-16

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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