STARLINK-11460 [DTC] (62069)

COSPAR: 2024-217N | Alt Name: Starlink 11460

Image
STARLINK-11460 [DTC] Satellite Image
Additional Sources
Launch Details

Launch Date

November 24, 2024

Launch Site

AFWTR

Launch Pad

SLC4E

Launch Vehicle

Falcon 9

Orbital Elements

NORAD ID

62069

International Designator

2024-217N

Epoch

Mon, 20 Jul 2026 05:05:59 GMT

Apogee

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Perigee

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Inclination

53.16°

Right Ascension

138.27°

Eccentricity

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Argument of Perigee

71.93°

Period

91.73 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-11460 [DTC]

Alternative Name

Starlink 11460

Type

Payload

Status

Operational

Owner

SPXS

Country

United States

Constellation

N/A

Related Satellites

Major Events

N/A

Latest TLEs
1 62069U 24217N   26201.21249250  .00122824  00000+0  10025-2 0  9993
2 62069  53.1570 138.2662 0001279  71.9336 288.1821 15.69739512 95925

Source: Celestrak

Summary
The satellite designated by NORAD CAT ID 62069 and OBJECT ID 2024-217N is a Starlink V2M model launched on November 24, 2024, from AFWTR SLC4E using the Falcon 9 launch vehicle. It has dimensions of 0.3 meters in length, 4.1 meters in diameter, and a span of 29 meters. The satellite's dry mass is 700 kilograms, with a total launch mass of 730 kilograms. Manufactured by SPXS (SpaceX), it belongs to the Starlink Group 9-13-13 payload and is part of the Starlink constellation network. Its shape consists of a box structure with a pan configuration, and its owner is SpaceX as well.

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 9-13-13

Purpose

Unknown

Mission

Unknown

Manufacturer

SPXS

Life Expectancy

Unknown

Bus

Starlink V2M

Configuration

Unknown

Motor

Unknown

Equipment

Unknown

Power System

Unknown

ADCS

Unknown

Transmitter Frequency

Unknown

Map
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