STARLINK-31099 (58781)

COSPAR: 2024-011S | Alt Name: Starlink 31099

Image
STARLINK-31099 Satellite Image
Additional Sources
Launch Details

Launch Date

January 14, 2024

Launch Site

AFWTR

Launch Pad

SLC4E

Launch Vehicle

Falcon 9

Orbital Elements

NORAD ID

58781

International Designator

2024-011S

Epoch

Sun, 19 Jul 2026 19:01:44 GMT

Apogee

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Perigee

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Inclination

53.16°

Right Ascension

120.22°

Eccentricity

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Argument of Perigee

81.53°

Period

94.11 min

Mean Motion

15.30 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-31099

Alternative Name

Starlink 31099

Type

Payload

Status

Operational

Owner

SPXS

Country

United States

Constellation

N/A

Related Satellites

Major Events

N/A

Latest TLEs
1 58781U 24011S   26200.79288176  .00001391  00000+0  59114-4 0  9992
2 58781  53.1587 120.2185 0001195  81.5274 278.5862 15.30188309140496

Source: Celestrak

Summary
The Starlink-31099 satellite, designated by NORAD as 58781 and cataloged under OBJECT_ID 2024-011S, is a part of the Starlink v2 Mini configuration manufactured by SpaceX (SPXS). Launched on January 14, 2024, from Space Launch Complex 4E (SLC4E) at AFWTR with a Falcon 9 launch vehicle, it weighs approximately 730 kg at launch and has a dry mass of 700 kg. The satellite features solar arrays and batteries for power generation and is equipped with Ku/Ka/E-band payload and optical inter-satellite link equipment. Its dimensions are 0.3 meters in length, 4.1 meters in diameter, and 29 meters in span, with an Argon ion thruster motor system for propulsion. The satellite is designed for communication purposes as part of the Starlink Group 7-10-17 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 7-10-17

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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