STARLINK-11098 [DTC] (59760)

COSPAR: 2024-091H | Alt Name: Starlink 11098

Image
STARLINK-11098 [DTC] Satellite Image
Additional Sources
Launch Details

Launch Date

May 14, 2024

Launch Site

AFWTR

Launch Pad

SLC4E

Launch Vehicle

Falcon 9

Orbital Elements

NORAD ID

59760

International Designator

2024-091H

Epoch

Sun, 19 Jul 2026 14:36:42 GMT

Apogee

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Perigee

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Inclination

53.16°

Right Ascension

275.88°

Eccentricity

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Argument of Perigee

87.83°

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-11098 [DTC]

Alternative Name

Starlink 11098

Type

Payload

Status

Operational

Owner

SPXS

Country

United States

Constellation

N/A

Related Satellites

Major Events

N/A

Latest TLEs
1 59760U 24091H   26200.60883068 -.00001131  00000+0 -44823-5 0  9995
2 59760  53.1591 275.8816 0001287  87.8261 272.2904 15.69681473126230

Source: Celestrak

Summary
The satellite named STARLINK-11098 [DTC] or Starlink 11098 is part of the Starlink v2 Mini constellation and was launched on May 14, 2024, from AFWTR SLC4E using a Falcon 9 launch vehicle. It has a length of 0.3 meters, 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. Its mission is communication, powered by solar arrays and batteries, and equipped with D2C payload and an optical inter-satellite link. The propulsion system uses Argon ion thrusters. It was manufactured by SPXS and owned by the same entity.

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 8-7-08

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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