STARLINK-31251 (58836)

COSPAR: 2024-017L | Alt Name: Starlink 31251

Image
STARLINK-31251 Satellite Image
Additional Sources
Launch Details

Launch Date

January 24, 2024

Launch Site

AFWTR

Launch Pad

SLC4E

Launch Vehicle

Falcon 9

Orbital Elements

NORAD ID

58836

International Designator

2024-017L

Epoch

Mon, 20 Jul 2026 06:00:04 GMT

Apogee

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Perigee

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Inclination

53.16°

Right Ascension

308.54°

Eccentricity

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Argument of Perigee

95.11°

Period

93.90 min

Mean Motion

15.34 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-31251

Alternative Name

Starlink 31251

Type

Payload

Status

Operational

Owner

SPXS

Country

United States

Constellation

N/A

Related Satellites

Major Events

N/A

Latest TLEs
1 58836U 24017L   26201.25004630  .00051605  00000+0  15702-2 0  9998
2 58836  53.1587 308.5411 0001073  95.1141 223.5656 15.33537500  5865

Source: Celestrak

Summary
The satellite STARLINK-31251, also known as Starlink 31251, is a communication satellite part of the Starlink Group 7-11-11 and was launched on January 24, 2024, from AFWTR's SLC4E launch pad using a Falcon 9 rocket. It has a configuration known as Starlink v2 Mini and measures approximately 0.3 meters in length with a diameter of 4.1 meters and spans 29 meters. The satellite weighs 700 kg dry, with an initial launch mass of 730 kg. Its equipment includes Ku/Ka/E-band payload and an optical inter-satellite link for communication purposes. Power is provided by solar arrays and batteries, while it uses Argon ion thrusters as its motor system. The satellite's shape is described as a box with pan configuration, and it was manufactured by SPXS (SpaceX).

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 7-11-11

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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