STARLINK-31663 (59576)

COSPAR: 2024-076N | Alt Name: Starlink 31663

Image
STARLINK-31663 Satellite Image
Additional Sources
Launch Details

Launch Date

April 23, 2024

Launch Pad

LC40

Launch Vehicle

Falcon 9

Orbital Elements

NORAD ID

59576

International Designator

2024-076N

Epoch

Sat, 18 Jul 2026 19:35:07 GMT

Apogee

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Perigee

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Inclination

43.00°

Right Ascension

348.73°

Eccentricity

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Argument of Perigee

257.64°

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-31663

Alternative Name

Starlink 31663

Type

Payload

Status

Operational

Owner

SPXS

Country

United States

Constellation

N/A

Related Satellites

Major Events

N/A

Latest TLEs
1 59576U 24076N   26199.81605404  .00000915  00000+0  42771-4 0  9995
2 59576  43.0035 348.7300 0001525 257.6436 102.4245 15.27580118126555

Source: Celestrak

Summary
The satellite identified by NORAD CAT ID 59576 and OBJECT ID 2024-076N is a Starlink V2M configuration named STARLINK-31663, launched on April 23, 2024, from the Cape Canaveral Space Force Station Launch Complex 40 using a Falcon 9 launch vehicle. It has dimensions of 0.3 meters in length and 4.1 meters in diameter with a span of 29 meters. The satellite's dry mass is 700 kilograms, and its launch mass was 730 kilograms. Equipped with a Ku/Ka/E-band payload and an optical inter-satellite link, it is designed for communication purposes using Argon ion thrusters for propulsion and solar arrays with batteries for power. The spacecraft has a box plus pan shape and is owned by SpaceX (SPXS).

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 6-53-13

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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