STARLINK-31630 (59271)

COSPAR: 2024-050T | Alt Name: Starlink 31630

Image
STARLINK-31630 Satellite Image
Additional Sources
Launch Details

Launch Date

March 19, 2024

Launch Site

AFWTR

Launch Pad

SLC4E

Launch Vehicle

Falcon 9

Orbital Elements

NORAD ID

59271

International Designator

2024-050T

Epoch

Sun, 19 Jul 2026 14:38:06 GMT

Apogee

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Perigee

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Inclination

53.16°

Right Ascension

273.50°

Eccentricity

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Argument of Perigee

64.77°

Period

93.85 min

Mean Motion

15.34 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-31630

Alternative Name

Starlink 31630

Type

Payload

Status

Partially operational

Owner

SPXS

Country

United States

Constellation

N/A

Related Satellites

Major Events

N/A

Latest TLEs
1 59271U 24050T   26200.60979409  .00001904  00000+0  67483-4 0  9994
2 59271  53.1600 273.4983 0000945  64.7732 295.3369 15.34390217130954

Source: Celestrak

Summary
The Starlink V2M satellite named STARLINK-31630 (OBJECT_ID: 2024-050T) was launched on March 19, 2024, from AFWTR SLC4E using a Falcon 9 launch vehicle. It measures 0.3 meters in length with a diameter of 4.1 meters and spans 29 meters when deployed. The satellite has a dry mass of 700 kg and launched with a total mass of 730 kg. Equipped with a Ku/Ka/E-band payload, optical inter-satellite link, and Argon ion thrusters for propulsion, it primarily serves communication purposes as part of the Starlink Group 7-16-18 constellation managed by SpaceX (SPXS). Power is supplied through solar arrays and batteries, and its shape consists of a box with a pan configuration.

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 7-16-18

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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