STARLINK-11175 [DTC] (60191)

COSPAR: 2024-124J | Alt Name: Starlink 11175

Image
STARLINK-11175 [DTC] Satellite Image
Additional Sources
Launch Details

Launch Date

July 3, 2024

Launch Pad

LC40

Launch Vehicle

Falcon 9

Orbital Elements

NORAD ID

60191

International Designator

2024-124J

Epoch

Sun, 19 Jul 2026 08:56:26 GMT

Apogee

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Perigee

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Inclination

53.16°

Right Ascension

232.30°

Eccentricity

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Argument of Perigee

81.35°

Period

91.74 min

Mean Motion

15.70 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-11175 [DTC]

Alternative Name

Starlink 11175

Type

Payload

Status

Operational

Owner

SPXS

Country

United States

Constellation

N/A

Related Satellites

Major Events

N/A

Latest TLEs
1 60191U 24124J   26200.37253389  .00001166  00000+0  14478-4 0  9991
2 60191  53.1582 232.3024 0000962  81.3485 278.7642 15.69707601117215

Source: Celestrak

Summary
The satellite STARLINK-11175 [DTC], also known as Starlink 11175, is a communication satellite manufactured by SPXS and launched on July 3, 2024, from LC40 at AFETR using a Falcon 9 launch vehicle. It belongs to the Starlink v2 Mini configuration with a BUS type of Starlink V2M. The spacecraft measures 0.3 meters in length, has a diameter of 4.1 meters, and spans 29 meters when deployed. Its dry mass is 700 kg, and it weighs 730 kg at launch. It is equipped with D2C payload and an optical inter-satellite link for communication purposes. The satellite uses Argon ion thrusters as its motor and solar arrays combined with batteries for power supply.

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 8-9-09

Purpose

Communication

Mission

Communication

Manufacturer

SPXS

Life Expectancy

Unknown

Bus

Starlink V2M

Configuration

Starlink v2 Mini

Motor

Argon ion thrusters

Equipment

D2C payload, optical inter-satellite link

Power System

Solar arrays, batteries

ADCS

Unknown

Transmitter Frequency

Unknown

Map
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