STARLINK-11081 [DTC] (60405)

COSPAR: 2024-141H | Alt Name: Starlink 11081

Image
STARLINK-11081 [DTC] Satellite Image
Additional Sources
Launch Details

Launch Date

August 10, 2024

Launch Pad

LC40

Launch Vehicle

Falcon 9

Orbital Elements

NORAD ID

60405

International Designator

2024-141H

Epoch

Sun, 19 Jul 2026 06:08:57 GMT

Apogee

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Perigee

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Inclination

53.16°

Right Ascension

157.92°

Eccentricity

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Argument of Perigee

86.18°

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-11081 [DTC]

Alternative Name

Starlink 11081

Type

Payload

Status

Operational

Owner

SPXS

Country

United States

Constellation

N/A

Related Satellites

Major Events

N/A

Latest TLEs
1 60405U 24141H   26200.25622174 -.00000090  00000+0  41189-5 0  9993
2 60405  53.1604 157.9247 0001098  86.1819 273.9324 15.69705870112352

Source: Celestrak

Summary
The satellite STARLINK-11081 [DTC], also known as Starlink 11081, is a communication satellite built by SPXS and launched on August 10, 2024, from Launch Complex 40 at the Air Force Eastern Test Range (AFETR) using a Falcon 9 launch vehicle. The satellite has a bus type of Starlink V2M with a configuration known as Starlink v2 Mini. It measures 0.3 meters in length and 4.1 meters in diameter, with a span of 29 meters. At launch, it had a mass of 730 kg, reducing to 700 kg dry mass. The satellite is equipped with direct-to-consumer (D2C) payload capabilities, an optical inter-satellite link, and Argon ion thrusters for propulsion. Power is supplied by solar arrays and batteries.

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 8-3-08

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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