STARLINK-31822 (59752)

COSPAR: 2024-090Y | Alt Name: Starlink 31822

Image
STARLINK-31822 Satellite Image
Additional Sources
Launch Details

Launch Date

May 13, 2024

Launch Pad

LC40

Launch Vehicle

Falcon 9

Orbital Elements

NORAD ID

59752

International Designator

2024-090Y

Epoch

Sun, 19 Jul 2026 06:15:41 GMT

Apogee

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Perigee

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Inclination

43.00°

Right Ascension

160.33°

Eccentricity

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Argument of Perigee

258.69°

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-31822

Alternative Name

Starlink 31822

Type

Payload

Status

Operational

Owner

SPXS

Country

United States

Constellation

N/A

Related Satellites

Major Events

N/A

Latest TLEs
1 59752U 24090Y   26200.26090162  .00000415  00000+0  24603-4 0  9997
2 59752  43.0011 160.3262 0000674 258.6944 101.3831 15.27578658123551

Source: Celestrak

Summary
The Starlink V2M satellite, designated STARLINK-31822 or Starlink 31822, is a communication satellite part of the Starlink v2 Mini configuration. Launched on May 13, 2024, from AFETR LC40 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 weighs 730 kilograms at launch and operates on solar arrays and batteries for power. It is equipped with Ku/Ka/E-band payload systems and optical inter-satellite links, and uses Argon ion thrusters as its propulsion system. Manufactured by SPXS and owned by the same entity, it serves a communication 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

0.3

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 6-58-23

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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