STARLINK-11129 [DTC] (60038)

COSPAR: 2024-112A | Alt Name: Starlink 11129

Image
STARLINK-11129 [DTC] Satellite Image
Additional Sources
Launch Details

Launch Date

June 8, 2024

Launch Site

AFWTR

Launch Pad

SLC4E

Launch Vehicle

Falcon 9

Orbital Elements

NORAD ID

60038

International Designator

2024-112A

Epoch

Sun, 19 Jul 2026 18:50:39 GMT

Apogee

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Perigee

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Inclination

53.16°

Right Ascension

335.41°

Eccentricity

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Argument of Perigee

135.91°

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-11129 [DTC]

Alternative Name

Starlink 11129

Type

Payload

Status

Operational

Owner

SPXS

Country

United States

Constellation

N/A

Related Satellites

Major Events

N/A

Latest TLEs
1 60038U 24112A   26200.78517810  .00000212  00000+0  65985-5 0  9996
2 60038  53.1598 335.4126 0000323 135.9103 224.1941 15.69709122121722

Source: Celestrak

Summary
The satellite named STARLINK-11129 [DTC], also known as Starlink 11129, is a Starlink v2 Mini configuration spacecraft manufactured by SPXS (SpaceX). It was launched on June 8, 2024, from AFWTR (Cape Canaveral Space Force Station) using Falcon 9 at SLC4E. The satellite has dimensions of 0.3 meters in length and a diameter of 4.1 meters with a span of 29 meters. It weighs 700 kg dry and had an initial launch mass of 730 kg. Equipped with D2C payload and optical inter-satellite link, the satellite utilizes solar arrays and batteries for power and Argon ion thrusters for propulsion. Its primary mission is communication within the Starlink Group 8-8-01 constellation.

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 8-8-01

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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