STARLINK-31846 (60126)

COSPAR: 2024-118P | Alt Name: Starlink 31846

Image
STARLINK-31846 Satellite Image
Additional Sources
Launch Details

Launch Date

June 24, 2024

Launch Site

AFWTR

Launch Pad

SLC4E

Launch Vehicle

Falcon 9

Orbital Elements

NORAD ID

60126

International Designator

2024-118P

Epoch

Mon, 20 Jul 2026 01:47:39 GMT

Apogee

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Perigee

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Inclination

53.16°

Right Ascension

131.20°

Eccentricity

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Argument of Perigee

81.68°

Period

94.01 min

Mean Motion

15.32 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-31846

Alternative Name

Starlink 31846

Type

Payload

Status

Operational

Owner

SPXS

Country

United States

Constellation

N/A

Related Satellites

Major Events

N/A

Latest TLEs
1 60126U 24118P   26201.07476051  .00000628  00000+0  32010-4 0  9997
2 60126  53.1596 131.2008 0001388  81.6815 278.4344 15.31703956115975

Source: Celestrak

Summary
The satellite STARLINK-31846 (OBJECT_ID: 2024-118P) is a Starlink v2 Mini configuration built by SPXS for communication purposes and launched on June 24, 2024, from AFWTR SLC4E using a Falcon 9 launch vehicle. It has dimensions of 0.3 meters in length, 4.1 meters in diameter, and spans 29 meters with solar arrays and batteries providing power. The satellite is equipped with a Ku/Ka/E-band payload, an optical inter-satellite link, and Argon ion thrusters for maneuvering. Its dry mass is 700 kg, and it weighed 730 kg at launch. It belongs to the Starlink Group 9-2-14 constellation and has a box shape 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 9-2-14

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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