STARLINK-11276 [DTC] (61244)

COSPAR: 2024-175B | Alt Name: Starlink 11276

Image
STARLINK-11276 [DTC] Satellite Image
Additional Sources
Launch Details

Launch Date

September 25, 2024

Launch Site

AFWTR

Launch Pad

SLC4E

Launch Vehicle

Falcon 9

Orbital Elements

NORAD ID

61244

International Designator

2024-175B

Epoch

Sun, 19 Jul 2026 05:01:53 GMT

Apogee

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Perigee

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Inclination

53.16°

Right Ascension

127.89°

Eccentricity

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Argument of Perigee

96.40°

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-11276 [DTC]

Alternative Name

Starlink 11276

Type

Payload

Status

Operational

Owner

SPXS

Country

United States

Constellation

N/A

Related Satellites

Major Events

N/A

Latest TLEs
1 61244U 24175B   26200.20965273  .00000529  00000+0  92258-5 0  9996
2 61244  53.1605 127.8884 0001011  96.3996 263.7137 15.69711438104023

Source: Celestrak

Summary
The STARLINK-11276 [DTC], also known as Starlink 11276, is a communication satellite belonging to the Starlink v2 Mini configuration and part of the Starlink Group 9-8-02 payload. Launched on September 25, 2024, from AFWTR SLC4E using a Falcon 9 launch vehicle, it has dimensions of 0.3 meters in length, a diameter of 4.1 meters, and a span of 29 meters. The satellite's dry mass is 700 kg with a launch mass of 730 kg. It was manufactured by SPXS for communication purposes and is equipped with D2C payload and optical inter-satellite link technology, powered by solar arrays and batteries. Propulsion is provided by Argon ion thrusters. The satellite's shape is described as box + pan.

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 9-8-02

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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