STARLINK-31407 (59250)

COSPAR: 2024-049V | Alt Name: Starlink 31407

Image
STARLINK-31407 Satellite Image
Additional Sources
Launch Details

Launch Date

March 16, 2024

Launch Pad

LC39A

Launch Vehicle

Falcon 9

Orbital Elements

NORAD ID

59250

International Designator

2024-049V

Epoch

Sun, 19 Jul 2026 04:00:47 GMT

Apogee

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Perigee

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Inclination

43.00°

Right Ascension

109.79°

Eccentricity

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Argument of Perigee

270.86°

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-31407

Alternative Name

Starlink 31407

Type

Payload

Status

Operational

Owner

SPXS

Country

United States

Constellation

N/A

Related Satellites

Major Events

N/A

Latest TLEs
1 59250U 24049V   26200.16721530  .00001440  00000+0  61833-4 0  9998
2 59250  43.0010 109.7881 0000874 270.8579  89.2173 15.27582891132635

Source: Celestrak

Summary
The Starlink-31407 satellite, designated OBJECT_ID 2024-049V, is a part of SpaceX's Starlink v2 Mini constellation. It was launched on March 16, 2024, from Kennedy Space Center LC39A using a Falcon 9 launch vehicle. The satellite has dimensions of 0.3 meters in length and 4.1 meters in diameter with a span of 29 meters. Weighing 730 kg at launch and 700 kg dry mass, it is equipped with a Ku/Ka/E-band payload and an optical inter-satellite link for communication purposes. It uses solar arrays and batteries for power generation and Argon ion thrusters for propulsion. The satellite's shape consists of a box and pan design.

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 6-44-20

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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