STARLINK-31963 (59893)

COSPAR: 2024-100J | Alt Name: Starlink 31963

Image
STARLINK-31963 Satellite Image
Additional Sources
Launch Details

Launch Date

May 28, 2024

Launch Pad

LC40

Launch Vehicle

Falcon 9

Orbital Elements

NORAD ID

59893

International Designator

2024-100J

Epoch

Mon, 20 Jul 2026 00:29:57 GMT

Apogee

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Perigee

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Inclination

43.00°

Right Ascension

98.20°

Eccentricity

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Argument of Perigee

260.34°

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-31963

Alternative Name

Starlink 31963

Type

Payload

Status

Operational

Owner

SPXS

Country

United States

Constellation

N/A

Related Satellites

Major Events

N/A

Latest TLEs
1 59893U 24100J   26201.02079999  .00000285  00000+0  19862-4 0  9991
2 59893  43.0015  98.1990 0000622 260.3445  99.7336 15.27575145121394

Source: Celestrak

Summary
The STARLINK-31963 satellite, also known as Starlink 31963, is a communication satellite built by SpaceX (SPXS) and launched on May 28, 2024, from the Air Force Eastern Test Range (AFETR), LC40 pad, using a Falcon 9 launch vehicle. It belongs to the Starlink V2M series with the Starlink v2 Mini configuration. The satellite measures 0.3 meters in length and has a diameter of 4.1 meters with a span of 29 meters. Its dry mass is 700 kg, while its launch mass was 730 kg. It is powered by solar arrays and batteries and equipped with Ku/Ka/E-band payload and an optical inter-satellite link. The satellite uses Argon ion thrusters for propulsion and has a box plus panel shape. Its mission purpose is to provide communication services as part of the Starlink Group 6-60-09 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 6-60-09

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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