STARLINK-31449 (58966)

COSPAR: 2024-031B | Alt Name: Starlink 31449

Image
STARLINK-31449 Satellite Image
Additional Sources
Launch Details

Launch Date

February 15, 2024

Launch Site

AFWTR

Launch Pad

SLC4E

Launch Vehicle

Falcon 9

Orbital Elements

NORAD ID

58966

International Designator

2024-031B

Epoch

Mon, 20 Jul 2026 06:00:04 GMT

Apogee

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Perigee

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Inclination

53.16°

Right Ascension

40.51°

Eccentricity

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Argument of Perigee

93.91°

Period

93.85 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-31449

Alternative Name

Starlink 31449

Type

Payload

Status

Operational

Owner

SPXS

Country

United States

Constellation

N/A

Related Satellites

Major Events

N/A

Latest TLEs
1 58966U 24031B   26201.25004630 -.00020202  00000+0 -58799-3 0  9993
2 58966  53.1597  40.5067 0001381  93.9072 324.2927 15.34419266  5815

Source: Celestrak

Summary
The STARLINK-31449 satellite, also known as Starlink 31449, is a communication satellite manufactured by SPXS and launched on February 15, 2024, from the AFWTR launch site using a Falcon 9 launch vehicle. It belongs to the Starlink v2 Mini configuration with dimensions of 0.3 meters in length, 4.1 meters in diameter, and has a span of 29 meters. The satellite's dry mass is 700 kg, and its launch mass was 730 kg. Equipped with a Ku/Ka/E-band payload and an optical inter-satellite link, it uses solar arrays and batteries for power and Argon ion thrusters as motors. Its shape consists of a box with a pan configuration.

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 7-14-02

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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