STARLINK-31959 (59925)

COSPAR: 2024-106D | Alt Name: Starlink 31959

Image
STARLINK-31959 Satellite Image
Additional Sources
Launch Details

Launch Date

June 1, 2024

Launch Pad

LC40

Launch Vehicle

Falcon 9

Orbital Elements

NORAD ID

59925

International Designator

2024-106D

Epoch

Sun, 19 Jul 2026 16:30:11 GMT

Apogee

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Perigee

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Inclination

43.00°

Right Ascension

303.23°

Eccentricity

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Argument of Perigee

257.04°

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-31959

Alternative Name

Starlink 31959

Type

Payload

Status

Operational

Owner

SPXS

Country

United States

Constellation

N/A

Related Satellites

Major Events

N/A

Latest TLEs
1 59925U 24106D   26200.68763140  .00001016  00000+0  46443-4 0  9990
2 59925  43.0021 303.2284 0001325 257.0385 103.0318 15.27579423120751

Source: Celestrak

Summary
The satellite STARLINK-31959 (OBJECT_ID: 2024-106D) is a Starlink v2 Mini model manufactured by SPXS and launched on June 1, 2024, from LC40 at AFETR using a Falcon 9 launch vehicle. It has dimensions of 0.3 meters in length, a diameter of 4.1 meters, and a span of 29 meters. The satellite's dry mass is 700 kilograms with a launch mass of 730 kilograms. Equipped with Ku/Ka/E-band payload and optical inter-satellite link, it uses Argon ion thrusters for propulsion and solar arrays along with batteries for power supply. Its mission and purpose are centered around 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 6-64-04

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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