STARLINK-31570 (59324)

COSPAR: 2024-057E | Alt Name: Starlink 31570

Image
STARLINK-31570 Satellite Image
Additional Sources
Launch Details

Launch Date

March 25, 2024

Launch Pad

LC40

Launch Vehicle

Falcon 9

Orbital Elements

NORAD ID

59324

International Designator

2024-057E

Epoch

Sun, 19 Jul 2026 21:29:01 GMT

Apogee

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Perigee

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Inclination

43.00°

Right Ascension

160.84°

Eccentricity

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Argument of Perigee

266.13°

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-31570

Alternative Name

Starlink 31570

Type

Payload

Status

Operational

Owner

SPXS

Country

United States

Constellation

N/A

Related Satellites

Major Events

N/A

Latest TLEs
1 59324U 24057E   26200.89515780 -.00001411  00000+0 -41746-4 0  9998
2 59324  43.0005 160.8367 0001228 266.1317  93.9394 15.27580728130058

Source: Celestrak

Summary
The STARLINK-31570 satellite, also known as Starlink 31570, is a communication satellite based on the Starlink v2 Mini configuration and part of the Starlink Group 6-46-05 payload. Launched by SpaceX (SPXS) from LC40 at AFETR using a Falcon 9 launch vehicle on March 25, 2024, it reached stable orbit on March 26, 2024. The satellite has dimensions of 0.3 meters in length and 4.1 meters in diameter with a span of 29 meters. It carries a Ku/Ka/E-band payload and an optical inter-satellite link for communication purposes. Equipped with solar arrays and batteries for power, it uses Argon ion thrusters as its motor system to maintain its orbit. The launch mass was 730 kg, with a dry mass of 700 kg.

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 6-46-05

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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