STARLINK-31674 (59517)

COSPAR: 2024-073G | Alt Name: Starlink 31674

Image
STARLINK-31674 Satellite Image
Additional Sources
Launch Details

Launch Date

April 17, 2024

Launch Pad

LC39A

Launch Vehicle

Falcon 9

Orbital Elements

NORAD ID

59517

International Designator

2024-073G

Epoch

Mon, 20 Jul 2026 06:34:03 GMT

Apogee

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Perigee

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Inclination

43.00°

Right Ascension

289.17°

Eccentricity

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Argument of Perigee

280.98°

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-31674

Alternative Name

Starlink 31674

Type

Payload

Status

Operational

Owner

SPXS

Country

United States

Constellation

N/A

Related Satellites

Major Events

N/A

Latest TLEs
1 59517U 24073G   26201.27365138 -.00000269  00000+0 -25239-6 0  9994
2 59517  43.0002 289.1690 0001046 280.9776  79.0958 15.27575546126456

Source: Celestrak

Summary
The satellite STARLINK-31674 (OBJECT_ID: 2024-073G) is a Starlink v2 Mini configuration launched on April 17, 2024, from Kennedy Space Center's LC39A using a Falcon 9 launch vehicle. It has a dry mass of 700 kg and measures 0.3 meters in length with a diameter of 4.1 meters and a span of 29 meters. The satellite is equipped with a Ku/Ka/E-band payload, an optical inter-satellite link, solar arrays, batteries, and Argon ion thrusters for propulsion. It is owned by SpaceX (SPXS) and serves communication purposes as part of the Starlink Group 6-51-07 constellation. The satellite's shape consists of a box with a pan configuration, and it was manufactured by SpaceX.

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 6-51-07

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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