STARLINK-31850 (59903)

COSPAR: 2024-100U | Alt Name: Starlink 31850

Image
STARLINK-31850 Satellite Image
Additional Sources
Launch Details

Launch Date

May 28, 2024

Launch Pad

LC40

Launch Vehicle

Falcon 9

Orbital Elements

NORAD ID

59903

International Designator

2024-100U

Epoch

Sun, 19 Jul 2026 17:28:54 GMT

Apogee

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Perigee

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Inclination

43.00°

Right Ascension

99.43°

Eccentricity

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Argument of Perigee

264.73°

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-31850

Alternative Name

Starlink 31850

Type

Payload

Status

Operational

Owner

SPXS

Country

United States

Constellation

N/A

Related Satellites

Major Events

N/A

Latest TLEs
1 59903U 24100U   26200.72841274  .00000516  00000+0  28277-4 0  9999
2 59903  43.0026  99.4270 0001206 264.7335  95.3379 15.27575692121293

Source: Celestrak

Summary
The Starlink-31850 satellite, also known as Starlink 31850, is a communication spacecraft under the Starlink v2 Mini configuration, part of the Starlink Group 6-60-19. Launched on May 28, 2024, from LC40 at AFETR using a Falcon 9 launch vehicle, it was manufactured by SPXS and owned by SPXS. The satellite has dimensions of 0.3 meters in length, 4.1 meters in diameter, and spans 29 meters. It carries a Ku/Ka/E-band payload and an optical inter-satellite link for communication purposes. Its dry mass is 700 kg with a launch mass of 730 kg. Power is provided by solar arrays and batteries. The satellite uses Argon ion thrusters as its propulsion system.

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 6-60-19

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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