STARLINK-11166 [DTC] (60062)

COSPAR: 2024-113D | Alt Name: Starlink 11166

Image
STARLINK-11166 [DTC] Satellite Image
Additional Sources
Launch Details

Launch Date

June 19, 2024

Launch Site

AFWTR

Launch Pad

SLC4E

Launch Vehicle

Falcon 9

Orbital Elements

NORAD ID

60062

International Designator

2024-113D

Epoch

Sun, 19 Jul 2026 13:27:55 GMT

Apogee

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Perigee

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Inclination

53.16°

Right Ascension

261.09°

Eccentricity

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Argument of Perigee

82.18°

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-11166 [DTC]

Alternative Name

Starlink 11166

Type

Payload

Status

Operational

Owner

SPXS

Country

United States

Constellation

N/A

Related Satellites

Major Events

N/A

Latest TLEs
1 60062U 24113D   26200.56105330 -.00000821  00000+0 -19195-5 0  9990
2 60062  53.1596 261.0924 0001058  82.1843 277.9295 15.69714077120279

Source: Celestrak

Summary
The satellite named STARLINK-11166 [DTC], or Starlink 11166, is a Starlink v2 Mini spacecraft (BUS: Starlink V2M) owned by SPXS and launched on June 19, 2024. It was deployed from SLC4E at AFWTR using a Falcon 9 launch vehicle. The satellite has dimensions of 0.3 meters in length, 4.1 meters in diameter, and a span of 29 meters. Its dry mass is 700 kilograms with a launch mass of 730 kilograms. It features D2C payload and optical inter-satellite link equipment and uses Argon ion thrusters for propulsion. The satellite is equipped with solar arrays and batteries for power generation and has a box plus pan shape. Its mission focuses on 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 9-1-04

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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