STARLINK-5766 (56025)

COSPAR: 2023-042AR | Alt Name: Starlink 5766

Image
STARLINK-5766 Satellite Image
Additional Sources
Launch Details

Launch Date

March 24, 2023

Launch Pad

LC40

Launch Vehicle

Falcon 9

Orbital Elements

NORAD ID

56025

International Designator

2023-042AR

Epoch

Sun, 19 Jul 2026 20:27:42 GMT

Apogee

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Perigee

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Inclination

43.00°

Right Ascension

19.21°

Eccentricity

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Argument of Perigee

273.82°

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-5766

Alternative Name

Starlink 5766

Type

Payload

Status

Operational

Owner

SPXS

Country

United States

Constellation

N/A

Related Satellites

Major Events

N/A

Latest TLEs
1 56025U 23042AR  26200.85257177  .00000460  00000+0  26241-4 0  9999
2 56025  43.0026  19.2142 0000917 273.8195  86.2552 15.27576322183242

Source: Celestrak

Summary
The STARLINK-5766 satellite, also known as Starlink 5766, is part of the Starlink constellation owned by SPXS (SpaceX). It was launched on March 24, 2023, from Cape Canaveral Air Force Station's LC40 launch pad using a Falcon 9 launch vehicle. The satellite has dimensions of 0.2 meters in length and 2.8 meters in diameter, with a span of 9 meters. Its dry mass is 290 kg and its launch mass was 305 kg. Equipped with a Ku/Ka-band payload and an optical inter-satellite link, it uses Krypton ion thrusters for propulsion and solar arrays with batteries for power generation. The satellite's primary mission is communication, serving as part of the Starlink Group 5-5-40 constellation.

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

0.2

Diameter

2.8

Span

9

Dry Mass

290

Launch Mass

305

Shape

Box + pan

Radar Cross Section

Unknown

Visual Magnitude

Unknown

Color

Unknown

Material Composition

Unknown

Technical Details

Payload

Starlink Group 5-5-40

Purpose

Communication

Mission

Communication

Manufacturer

SPXS

Life Expectancy

Unknown

Bus

Starlink

Configuration

Unknown

Motor

Krypton ion thrusters

Equipment

Ku/Ka-band payload, optical inter-satellite link

Power System

Solar arrays, batteries

ADCS

Unknown

Transmitter Frequency

Unknown

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