STARLINK-31569 (59857)

COSPAR: 2024-097Y | Alt Name: Starlink 31569

Image
STARLINK-31569 Satellite Image
Additional Sources
Launch Details

Launch Date

May 23, 2024

Launch Pad

LC40

Launch Vehicle

Falcon 9

Orbital Elements

NORAD ID

59857

International Designator

2024-097Y

Epoch

Sun, 19 Jul 2026 19:40:58 GMT

Apogee

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Perigee

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Inclination

43.00°

Right Ascension

248.22°

Eccentricity

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Argument of Perigee

277.97°

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-31569

Alternative Name

Starlink 31569

Type

Payload

Status

Operational

Owner

SPXS

Country

United States

Constellation

N/A

Related Satellites

Major Events

N/A

Latest TLEs
1 59857U 24097Y   26200.82011750  .00001228  00000+0  54139-4 0  9998
2 59857  43.0015 248.2248 0001330 277.9675  82.1026 15.27585308122120

Source: Celestrak

Summary
The Starlink V2M satellite, designated STARLINK-31569 or Starlink 31569, is a communication satellite launched on May 23, 2024, from Launch Complex 40 at Cape Canaveral Air Force Station using a Falcon 9 launch vehicle. The spacecraft has dimensions of 0.3 meters in length and 4.1 meters in diameter with a span of 29 meters. It weighs 730 kg at launch and has a dry mass of 700 kg. 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. Manufactured by SPXS (SpaceX), it operates in a configuration known as Starlink v2 Mini and belongs to the Starlink Group 6-62-23 mission, aimed at enhancing global communication services.

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 6-62-23

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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