STARLINK-11188 [DTC] (60722)

COSPAR: 2024-152C | Alt Name: Starlink 11188

Image
STARLINK-11188 [DTC] Satellite Image
Additional Sources
Launch Details

Launch Date

August 28, 2024

Launch Pad

LC40

Launch Vehicle

Falcon 9

Orbital Elements

NORAD ID

60722

International Designator

2024-152C

Epoch

Sun, 19 Jul 2026 16:26:03 GMT

Apogee

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Perigee

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Inclination

53.16°

Right Ascension

185.77°

Eccentricity

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Argument of Perigee

103.67°

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-11188 [DTC]

Alternative Name

Starlink 11188

Type

Payload

Status

Operational

Owner

SPXS

Country

United States

Constellation

N/A

Related Satellites

Major Events

N/A

Latest TLEs
1 60722U 24152C   26200.68476580  .00001260  00000+0  15273-4 0  9995
2 60722  53.1593 185.7699 0001290 103.6653 256.4508 15.69692937109687

Source: Celestrak

Summary
The satellite named STARLINK-11188 [DTC], also known as Starlink 11188, is a communication satellite belonging to the Starlink v2 Mini configuration under the Bus model of Starlink V2M. Launched on August 28, 2024, from Launch Pad LC40 at AFETR using a Falcon 9 launch vehicle, this spacecraft was manufactured by SPXS and has an owner listed as SPXS. It features D2C payload and optical inter-satellite link equipment for its communication mission. The satellite has dimensions of 0.3 meters in length and 4.1 meters in diameter with a span of 29 meters, weighing 730 kg at launch and 700 kg dry mass. It is powered by solar arrays and batteries and uses Argon ion thrusters for propulsion. The shape of the satellite is described as Box + pan without additional details on its color or specific material composition provided in the data.

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 8-6-03

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

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