STARLINK-31462 (59466)

COSPAR: 2024-068M | Alt Name: Starlink 31462

Image
STARLINK-31462 Satellite Image
Additional Sources
Launch Details

Launch Date

April 10, 2024

Launch Pad

LC40

Launch Vehicle

Falcon 9

Orbital Elements

NORAD ID

59466

International Designator

2024-068M

Epoch

Sun, 19 Jul 2026 20:03:46 GMT

Apogee

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Perigee

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Inclination

43.00°

Right Ascension

8.13°

Eccentricity

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Argument of Perigee

268.03°

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-31462

Alternative Name

Starlink 31462

Type

Payload

Status

Operational

Owner

SPXS

Country

United States

Constellation

N/A

Related Satellites

Major Events

N/A

Latest TLEs
1 59466U 24068M   26200.83595207 -.00001129  00000+0 -31518-4 0  9995
2 59466  43.0029   8.1347 0001140 268.0283  92.0438 15.27565391128739

Source: Celestrak

Summary
STARLINK-31462 is a communication satellite under the Starlink v2 Mini configuration, launched on April 10, 2024, from Cape Canaveral Air Force Station's LC40 using a Falcon 9 launch vehicle. The spacecraft measures approximately 0.3 meters in length and has a diameter of 4.1 meters with a span of 29 meters. It carries a Ku/Ka/E-band payload along with an optical inter-satellite link, powered by solar arrays and batteries. Its dry mass is 700 kg, with a launch mass of 730 kg. The satellite is equipped with Argon ion thrusters for propulsion and was manufactured by SpaceX (SPXS) for communication purposes within the Starlink Group 6-48-12 constellation.

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 6-48-12

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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