STARLINK-31953 (59898)

COSPAR: 2024-100P | Alt Name: Starlink 31953

Image
STARLINK-31953 Satellite Image
Additional Sources
Launch Details

Launch Date

May 28, 2024

Launch Pad

LC40

Launch Vehicle

Falcon 9

Orbital Elements

NORAD ID

59898

International Designator

2024-100P

Epoch

Sun, 19 Jul 2026 02:23:12 GMT

Apogee

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Perigee

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Inclination

43.00°

Right Ascension

99.87°

Eccentricity

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Argument of Perigee

276.56°

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-31953

Alternative Name

Starlink 31953

Type

Payload

Status

Operational

Owner

SPXS

Country

United States

Constellation

N/A

Related Satellites

Major Events

N/A

Latest TLEs
1 59898U 24100P   26200.09944841  .00000745  00000+0  36593-4 0  9990
2 59898  43.0024  99.8661 0000829 276.5560  83.5198 15.27579323121296

Source: Celestrak

Summary
STARLINK-31953 is a Starlink v2 Mini communication satellite launched on May 28, 2024, from Launch Complex 40 at Cape Canaveral Space Force Station using a Falcon 9 launch vehicle. The satellite has dimensions of 0.3 meters in length and 4.1 meters in diameter with a span of 29 meters. It has a dry mass of 700 kg and a launch mass of 730 kg, powered by solar arrays and batteries. Equipped with Ku/Ka/E-band payload and an optical inter-satellite link, it also features Argon ion thrusters for propulsion. The satellite is owned and operated by SpaceX as part of the Starlink Group 6-60-14 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 6-60-14

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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