STARLINK-3983 (52618)

COSPAR: 2022-052W | Alt Name: Starlink 3983

Image

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Launch Details

Launch Date

May 14, 2022

Launch Site

Cape Canaveral Space Force Station

Launch Pad

LC40

Launch Vehicle

Falcon 9

Orbital Elements

NORAD ID

52618

International Designator

2022-052W

Epoch

Sun, 19 Jul 2026 20:00:01 GMT

Apogee

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Perigee

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Inclination

53.16°

Right Ascension

34.98°

Eccentricity

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Argument of Perigee

58.41°

Period

94.75 min

Mean Motion

15.20 rev/day

Latitude

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Longitude

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Altitude

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Velocity

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Polar Plot

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Starlink bus SpaceX Starlink constellation United States satellites Payloads

Basic Satellite Info

Name

STARLINK-3983

Alternative Name

Starlink 3983

Type

Payload

Status

Operational

Owner

SPXS

Country

United States

Constellation

N/A

Related Satellites

Major Events

N/A

Latest TLEs

1 52618U 22052W   26200.83335647  .00028394  00000+0  13204-2 0  9999

2 52618  53.1610  34.9829 0000719  58.4130 280.4705 15.19769641  5845

Source: Celestrak

Summary

STARLINK-3983 is a Starlink satellite launched by SpaceX on May 14, 2022, from Cape Canaveral Air Force Station Launch Complex 40 using a Falcon 9 launch vehicle. It measures 0.2 meters in length and has a diameter of 2.8 meters with a span of 9 meters. The satellite has a dry mass of 275 kilograms and launched at a mass of 297 kilograms. Equipped with Ku/Ka-band payload and an optical inter-satellite link, it utilizes krypton ion thrusters for propulsion and solar arrays with batteries for power. Its purpose is communication as part of the Starlink Group 4-15-21 constellation mission.

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

Dry Mass

275

Launch Mass

297

Shape

Box + pan

Radar Cross Section

Unknown

Visual Magnitude

Unknown

Color

Unknown

Material Composition

Unknown

Technical Details

Payload

Starlink Group 4-15-21

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

Map

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