STARLINK-31815 (59801)

COSPAR: 2024-093V | Alt Name: Starlink 31815

Image
STARLINK-31815 Satellite Image
Additional Sources
Launch Details

Launch Date

May 18, 2024

Launch Pad

LC40

Launch Vehicle

Falcon 9

Orbital Elements

NORAD ID

59801

International Designator

2024-093V

Epoch

Sun, 19 Jul 2026 20:01:58 GMT

Apogee

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Perigee

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Inclination

43.00°

Right Ascension

182.75°

Eccentricity

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Argument of Perigee

259.46°

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-31815

Alternative Name

Starlink 31815

Type

Payload

Status

Operational

Owner

SPXS

Country

United States

Constellation

N/A

Related Satellites

Major Events

N/A

Latest TLEs
1 59801U 24093V   26200.83470663  .00000735  00000+0  36210-4 0  9998
2 59801  43.0013 182.7487 0000874 259.4555 100.6198 15.27577321122906

Source: Celestrak

Summary
The STARLINK-31815 satellite, also known as Starlink 31815, is a communication satellite belonging to the Starlink v2 Mini configuration and was launched on May 18, 2024, from LC40 at AFETR using a Falcon 9 launch vehicle. It has dimensions of 0.3 meters in length, 4.1 meters in diameter, and spans 29 meters when fully deployed. The satellite is equipped with a Ku/Ka/E-band payload and an optical inter-satellite link for communication purposes. Its dry mass is 700 kilograms, while its launch mass was 730 kilograms, powered by solar arrays and batteries. It is operated by SPXS and uses Argon ion thrusters as its propulsion system.

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 6-59-20

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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