STARLINK-31713 (59381)

COSPAR: 2024-062H | Alt Name: Starlink 31713

Image
STARLINK-31713 Satellite Image
Additional Sources
Launch Details

Launch Date

April 2, 2024

Launch Site

AFWTR

Launch Pad

SLC4E

Launch Vehicle

Falcon 9

Orbital Elements

NORAD ID

59381

International Designator

2024-062H

Epoch

Sun, 19 Jul 2026 17:54:10 GMT

Apogee

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Perigee

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Inclination

53.16°

Right Ascension

2.72°

Eccentricity

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Argument of Perigee

96.57°

Period

93.85 min

Mean Motion

15.34 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-31713

Alternative Name

Starlink 31713

Type

Payload

Status

Operational

Owner

SPXS

Country

United States

Constellation

N/A

Related Satellites

Major Events

N/A

Latest TLEs
1 59381U 24062H   26200.74595796  .00001328  00000+0  50438-4 0  9999
2 59381  53.1611   2.7203 0000992  96.5677 263.5438 15.34401023129847

Source: Celestrak

Summary
The STARLINK-31713 satellite, also known as Starlink 31713, is a communication spacecraft belonging to the Starlink Group 7-18-08 and was launched on April 2, 2024, from AFWTR SLC4E using a Falcon 9 launch vehicle. It has a configuration of Starlink v2 Mini with dimensions of 0.3 meters in length and 4.1 meters in diameter, featuring a span of 29 meters. The satellite's dry mass is 700 kg, and its total launch mass was 730 kg. Equipped with Ku/Ka/E-band payload, optical inter-satellite link, and solar arrays for power, it uses Argon ion thrusters as its motor system. Manufactured by SPXS, the satellite's primary purpose is communication.

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 7-18-08

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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