STARLINK-11210 [DTC] (60116)

COSPAR: 2024-118D | Alt Name: Starlink 11210

Image
STARLINK-11210 [DTC] Satellite Image
Additional Sources
Launch Details

Launch Date

June 24, 2024

Launch Site

AFWTR

Launch Pad

SLC4E

Launch Vehicle

Falcon 9

Orbital Elements

NORAD ID

60116

International Designator

2024-118D

Epoch

Sun, 19 Jul 2026 11:59:48 GMT

Apogee

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Perigee

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Inclination

53.16°

Right Ascension

291.63°

Eccentricity

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Argument of Perigee

86.79°

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-11210 [DTC]

Alternative Name

Starlink 11210

Type

Payload

Status

Operational

Owner

SPXS

Country

United States

Constellation

N/A

Related Satellites

Major Events

N/A

Latest TLEs
1 60116U 24118D   26200.49986884  .00000233  00000+0  67826-5 0  9997
2 60116  53.1597 291.6343 0000942  86.7938 273.3188 15.69704515118690

Source: Celestrak

Summary
The satellite named STARLINK-11210 [DTC], also known as Starlink 11210, is a Starlink v2 Mini configuration spacecraft launched on June 24, 2024, from AFWTR Launch Site SLC4E using the Falcon 9 launch vehicle. The satellite measures 0.3 meters in length and has a diameter of 4.1 meters with a span of 29 meters. It weighs 730 kg at launch and 700 kg dry mass, operated by SPXS for communication purposes. Equipped with D2C payload and optical inter-satellite link, it utilizes Argon ion thrusters as its motor system and is powered by solar arrays and batteries. The satellite was stabilized on June 24, 2024, at 04:47:19 UTC and is part of the Starlink Group 9-2-04 payload mission.

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 9-2-04

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

Map
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