STARLINK-31515 (59476)

COSPAR: 2024-068X | Alt Name: Starlink 31515

Image
STARLINK-31515 Satellite Image
Additional Sources
Launch Details

Launch Date

April 10, 2024

Launch Pad

LC40

Launch Vehicle

Falcon 9

Orbital Elements

NORAD ID

59476

International Designator

2024-068X

Epoch

Sun, 19 Jul 2026 20:09:18 GMT

Apogee

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Perigee

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Inclination

43.00°

Right Ascension

8.18°

Eccentricity

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Argument of Perigee

279.41°

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-31515

Alternative Name

Starlink 31515

Type

Payload

Status

Operational

Owner

SPXS

Country

United States

Constellation

N/A

Related Satellites

Major Events

N/A

Latest TLEs
1 59476U 24068X   26200.83979897  .00000574  00000+0  30386-4 0  9990
2 59476  43.0026   8.1759 0001176 279.4059  80.6660 15.27572146128736

Source: Celestrak

Summary
STARLINK-31515 is a Starlink v2 Mini satellite (BUS: Starlink V2M) owned and operated by SpaceX (SPXS), launched on April 10, 2024, from Cape Canaveral Air Force Station's Launch Complex 40 using the Falcon 9 launch vehicle. The satellite has dimensions of 0.3 meters in length, a diameter of 4.1 meters, and a span of 29 meters. Its dry mass is 700 kg with a total launch mass of 730 kg. It is equipped with Ku/Ka/E-band payload systems, an optical inter-satellite link, solar arrays for power generation, batteries, Argon ion thrusters for propulsion, and serves the purpose of communication as part of the Starlink Group 6-48-22 constellation. The satellite has a shape described as "Box + pan" configuration.

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 6-48-22

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

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