STARLINK-4008 (52622)

COSPAR: 2022-052AA | Alt Name: Starlink 4008

Image
STARLINK-4008 Satellite Image
Additional Sources
Launch Details

Launch Date

May 14, 2022

Launch Pad

LC40

Launch Vehicle

Falcon 9

Orbital Elements

NORAD ID

52622

International Designator

2022-052AA

Epoch

Sun, 19 Jul 2026 20:00:01 GMT

Apogee

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Perigee

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Inclination

53.16°

Right Ascension

49.23°

Eccentricity

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Argument of Perigee

14.83°

Period

94.52 min

Mean Motion

15.23 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-4008

Alternative Name

Starlink 4008

Type

Payload

Status

Operational

Owner

SPXS

Country

United States

Constellation

N/A

Related Satellites

Major Events

N/A

Latest TLEs
1 52622U 22052AA  26200.83335647  .00022466  00000+0  94105-3 0  9998
2 52622  53.1613  49.2289 0000646  14.8274 250.8428 15.23475132  5786

Source: Celestrak

Summary
The STARLINK-4008 satellite, also known as Starlink 4008, is a communication satellite belonging to the Starlink constellation and was launched on May 14, 2022, from Cape Canaveral Air Force Station (AFETR), LC40, using a Falcon 9 launch vehicle. It has dimensions of approximately 0.2 meters in length, 2.8 meters in diameter, and spans about 9 meters when fully deployed. The satellite has a dry mass of 275 kilograms and a launch mass of 297 kilograms. Equipped with a Ku/Ka-band payload and an optical inter-satellite link, it utilizes krypton ion thrusters for propulsion and solar arrays along with batteries for power generation. Manufactured by SpaceX (SPXS), its primary purpose is to provide communication services as part of the Starlink Group 4-15-25 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

275

Launch Mass

297

Shape

Box + pan

Radar Cross Section

Unknown

Visual Magnitude

Unknown

Color

Unknown

Material Composition

Unknown

Technical Details

Payload

Starlink Group 4-15-25

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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