STARLINK-31616 (59270)

COSPAR: 2024-050S | Alt Name: Starlink 31616

Image
STARLINK-31616 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

59270

International Designator

2024-050S

Epoch

Sun, 19 Jul 2026 15:30:24 GMT

Apogee

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Perigee

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Inclination

53.16°

Right Ascension

287.22°

Eccentricity

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Argument of Perigee

99.93°

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-31616

Alternative Name

Starlink 31616

Type

Payload

Status

Operational

Owner

SPXS

Country

United States

Constellation

N/A

Related Satellites

Major Events

N/A

Latest TLEs
1 59270U 24050S   26200.64611307 -.00000624  00000+0 -73398-5 0  9990
2 59270  53.1610 287.2199 0001294  99.9328 260.1821 15.34391651130760

Source: Celestrak

Summary
The satellite STARLINK-31616 (OBJECT_ID: 2024-050S) is a Starlink v2 Mini communication satellite launched on March 19, 2024, from AFWTR SLC4E using the Falcon 9 launch vehicle. It has dimensions of 0.3 meters in length and 4.1 meters in diameter with a span of 29 meters, featuring solar arrays and batteries for power. The satellite weighs 730 kg at launch and its dry mass is 700 kg. Equipped with Ku/Ka/E-band payload and an optical inter-satellite link, it also utilizes Argon ion thrusters as its motor system. Manufactured by SPXS (SpaceX), this satellite operates in a box + pan shape configuration for communication purposes.

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 7-16-17

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

Map
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