STARLINK-31884 (59676)

COSPAR: 2024-084Y | Alt Name: Starlink 31884

Image
STARLINK-31884 Satellite Image
Additional Sources
Launch Details

Launch Date

May 6, 2024

Launch Pad

LC40

Launch Vehicle

Falcon 9

Orbital Elements

NORAD ID

59676

International Designator

2024-084Y

Epoch

Sun, 19 Jul 2026 20:04:18 GMT

Apogee

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Perigee

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Inclination

43.00°

Right Ascension

15.49°

Eccentricity

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Argument of Perigee

277.37°

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-31884

Alternative Name

Starlink 31884

Type

Payload

Status

Operational

Owner

SPXS

Country

United States

Constellation

N/A

Related Satellites

Major Events

N/A

Latest TLEs
1 59676U 24084Y   26200.83632758  .00006395  00000+0  24169-3 0  9990
2 59676  43.0001  15.4874 0001255 277.3675  82.7034 15.27582140124581

Source: Celestrak

Summary
STARLINK-31884 is a Starlink V2M satellite (Starlink v2 Mini configuration) owned and operated by SpaceX (SPXS). Launched on May 6, 2024, from the Cape Canaveral Space Force Station, LC40, aboard a Falcon 9 launch vehicle, it has dimensions of 0.3 meters in length, 4.1 meters in diameter, and spans 29 meters with its solar arrays extended. The satellite has a dry mass of 700 kg and a launch mass of 730 kg. It is equipped with Ku/Ka/E-band payload and optical inter-satellite link for communication purposes. Propulsion is provided by Argon ion thrusters, while power is generated through solar arrays and batteries. The satellite was successfully stabilized on May 6, 2024, at 19:19 UTC.

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 6-57-23

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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