STARLINK-31256 (59161)

COSPAR: 2024-044K | Alt Name: Starlink 31256

Image
STARLINK-31256 Satellite Image
Additional Sources
Launch Details

Launch Date

March 4, 2024

Launch Pad

LC40

Launch Vehicle

Falcon 9

Orbital Elements

NORAD ID

59161

International Designator

2024-044K

Epoch

Sun, 19 Jul 2026 22:20:08 GMT

Apogee

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Perigee

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Inclination

43.00°

Right Ascension

79.89°

Eccentricity

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Argument of Perigee

273.28°

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-31256

Alternative Name

Starlink 31256

Type

Payload

Status

Operational

Owner

SPXS

Country

United States

Constellation

N/A

Related Satellites

Major Events

N/A

Latest TLEs
1 59161U 24044K   26200.93065037  .00000190  00000+0  16441-4 0  9998
2 59161  43.0048  79.8923 0001412 273.2845  86.7845 15.27577322133826

Source: Celestrak

Summary
STARLINK-31256 is a communication satellite belonging to SpaceX's Starlink v2 Mini configuration. Launched on March 4, 2024, from LC40 at AFETR using a Falcon 9 launch vehicle, it has a length of 0.3 meters, a diameter of 4.1 meters, and a span of 29 meters. The satellite's dry mass is 700 kg with a launch mass of 730 kg. It is powered by solar arrays and batteries and equipped with a Ku/Ka/E-band payload and an optical inter-satellite link for communication purposes. Its propulsion system includes Argon ion thrusters, and it was deployed as part of the Starlink Group 6-41-10 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 6-41-10

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

Map
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