STARLINK-31866 (59668)

COSPAR: 2024-084Q | Alt Name: Starlink 31866

Image
STARLINK-31866 Satellite Image
Additional Sources
Launch Details

Launch Date

May 6, 2024

Launch Pad

LC40

Launch Vehicle

Falcon 9

Orbital Elements

NORAD ID

59668

International Designator

2024-084Q

Epoch

Sun, 19 Jul 2026 19:17:35 GMT

Apogee

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Perigee

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Inclination

43.00°

Right Ascension

8.28°

Eccentricity

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Argument of Perigee

266.76°

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-31866

Alternative Name

Starlink 31866

Type

Payload

Status

Operational

Owner

SPXS

Country

United States

Constellation

N/A

Related Satellites

Major Events

N/A

Latest TLEs
1 59668U 24084Q   26200.80388469  .00000041  00000+0  11023-4 0  9993
2 59668  43.0022   8.2841 0001344 266.7649  93.3049 15.27573364124662

Source: Celestrak

Summary
The STARLINK-31866 satellite, also known as Starlink 31866, is a communication satellite belonging to the Starlink v2 Mini configuration under the Starlink V2M bus series. Launched on May 6, 2024, from Cape Canaveral Air Force Station Launch Complex 40 (LC40) aboard a Falcon 9 launch vehicle, this satellite has dimensions of 0.3 meters in length and 4.1 meters in diameter with a span of 29 meters. Its 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 utilizes solar arrays and batteries for power. The satellite's propulsion system consists of Argon ion thrusters, enabling precise maneuvering in orbit. Manufactured by SpaceX (SPXS), the mission of STARLINK-31866 is to provide communication services as part of the Starlink Group 6-57-15 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 6-57-15

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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