STARLINK-31322 (59168)

COSPAR: 2024-044S | Alt Name: Starlink 31322

Image
STARLINK-31322 Satellite Image
Additional Sources
Launch Details

Launch Date

March 4, 2024

Launch Pad

LC40

Launch Vehicle

Falcon 9

Orbital Elements

NORAD ID

59168

International Designator

2024-044S

Epoch

Sun, 19 Jul 2026 17:11:58 GMT

Apogee

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Perigee

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Inclination

43.00°

Right Ascension

81.73°

Eccentricity

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Argument of Perigee

269.30°

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-31322

Alternative Name

Starlink 31322

Type

Payload

Status

Operational

Owner

SPXS

Country

United States

Constellation

N/A

Related Satellites

Major Events

N/A

Latest TLEs
1 59168U 24044S   26200.71664492  .00001015  00000+0  46395-4 0  9999
2 59168  43.0036  81.7265 0000964 269.3017  90.7724 15.27583214133782

Source: Celestrak

Summary
STARLINK-31322 is a communication satellite belonging to the Starlink v2 Mini configuration series under the Starlink Group 6-41-17 mission. Launched on March 4, 2024, from Launch Complex 40 at Cape Canaveral Air Force Station using a Falcon 9 launch vehicle, it has an object ID of 2024-044S and NORAD CAT ID of 59168. The satellite measures 0.3 meters in length with a diameter of 4.1 meters and a span of 29 meters, featuring solar arrays and batteries for power. It weighs approximately 700 kg dry and had a launch mass of 730 kg. Equipped with Ku/Ka/E-band payload and optical inter-satellite links, it uses Argon ion thrusters as its propulsion system. The satellite is owned by SpaceX (SPXS) and was manufactured by the same entity.

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 6-41-17

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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