STARLINK-31808 (59751)

COSPAR: 2024-090X | Alt Name: Starlink 31808

Image
STARLINK-31808 Satellite Image
Additional Sources
Launch Details

Launch Date

May 13, 2024

Launch Pad

LC40

Launch Vehicle

Falcon 9

Orbital Elements

NORAD ID

59751

International Designator

2024-090X

Epoch

Sun, 19 Jul 2026 21:25:48 GMT

Apogee

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Perigee

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Inclination

43.00°

Right Ascension

156.47°

Eccentricity

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Argument of Perigee

272.23°

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-31808

Alternative Name

Starlink 31808

Type

Payload

Status

Operational

Owner

SPXS

Country

United States

Constellation

N/A

Related Satellites

Major Events

N/A

Latest TLEs
1 59751U 24090X   26200.89292556  .00000564  00000+0  30027-4 0  9998
2 59751  43.0021 156.4708 0001263 272.2294  87.8413 15.27578478123652

Source: Celestrak

Summary
The Starlink V2M satellite, designated STARLINK-31808 (OBJECT_ID: 2024-090X), is a communication satellite launched on May 13, 2024, from the Cape Canaveral Space Force Station Launch Complex 40 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 has a dry mass of 700 kg and was manufactured by SpaceX (SPXS). Equipped with a Ku/Ka/E-band payload and an optical inter-satellite link, the satellite is powered by solar arrays and batteries. Its motor consists of Argon ion thrusters, and it belongs to the Starlink Group 6-58-22 constellation, serving as part of SpaceX's broader communication mission in space.

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 6-58-22

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

Map
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