STARLINK-31333 (58971)

COSPAR: 2024-031G | Alt Name: Starlink 31333

Image
STARLINK-31333 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

58971

International Designator

2024-031G

Epoch

Mon, 20 Jul 2026 06:00:04 GMT

Apogee

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Perigee

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Inclination

53.16°

Right Ascension

28.35°

Eccentricity

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Argument of Perigee

69.72°

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-31333

Alternative Name

Starlink 31333

Type

Payload

Status

Operational

Owner

SPXS

Country

United States

Constellation

N/A

Related Satellites

Major Events

N/A

Latest TLEs
1 58971U 24031G   26201.25004630 -.00006580  00000+0 -18889-3 0  9998
2 58971  53.1602  28.3495 0001198  69.7220  29.9008 15.33554383  5862

Source: Celestrak

Summary
The STARLINK-31333 satellite, also known as Starlink 31333, is a Starlink v2 Mini model launched on February 15, 2024, from AFWTR SLC4E using a Falcon 9 launch vehicle. Manufactured by SPXS, it has dimensions of 0.3 meters in length and a diameter of 4.1 meters with a span of 29 meters. The satellite weighs 700 kilograms dry and had a launch mass of 730 kilograms. Equipped with Ku/Ka/E-band payload and an optical inter-satellite link, it also features Argon ion thrusters for propulsion and solar arrays with batteries for power generation. Its mission is to provide communication services as part of the Starlink Group 7-14-07 constellation.

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 7-14-07

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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