STARLINK-11083 [DTC] (59424)

COSPAR: 2024-065D | Alt Name: Starlink 11083

Image
STARLINK-11083 [DTC] Satellite Image
Additional Sources
Launch Details

Launch Date

April 7, 2024

Launch Site

AFWTR

Launch Pad

SLC4E

Launch Vehicle

Falcon 9

Orbital Elements

NORAD ID

59424

International Designator

2024-065D

Epoch

Sun, 19 Jul 2026 14:57:01 GMT

Apogee

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Perigee

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Inclination

53.16°

Right Ascension

163.58°

Eccentricity

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Argument of Perigee

82.34°

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-11083 [DTC]

Alternative Name

Starlink 11083

Type

Payload

Status

Operational

Owner

SPXS

Country

United States

Constellation

N/A

Related Satellites

Major Events

N/A

Latest TLEs
1 59424U 24065D   26200.62293068  .00000323  00000+0  75312-5 0  9997
2 59424  53.1606 163.5808 0001307  82.3356 277.7811 15.69703238132199

Source: Celestrak

Summary
STARLINK-11083 [DTC], also known as Starlink 11083, is a communication satellite part of the Starlink v2 Mini configuration. Launched on April 7, 2024, from AFWTR SLC4E using a Falcon 9 launch vehicle, it has a dry mass of 700 kg and a launch mass of 730 kg. The satellite measures 0.3 meters in length with a diameter of 4.1 meters and a span of 29 meters. Equipped with D2C payload and an optical inter-satellite link, it uses Argon ion thrusters for propulsion and solar arrays along with batteries for power. Manufactured by SPXS (SpaceX), the satellite is owned by SpaceX and operates within the Starlink Group 8-1-04 payload group.

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 8-1-04

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

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