STARLINK-11510 [DTC] (62516)

COSPAR: 2025-004F | Alt Name: Starlink 11510

Image
STARLINK-11510 [DTC] Satellite Image
Additional Sources
Launch Details

Launch Date

January 8, 2025

Launch Pad

LC39A

Launch Vehicle

Falcon 9

Orbital Elements

NORAD ID

62516

International Designator

2025-004F

Epoch

Sun, 19 Jul 2026 11:39:37 GMT

Apogee

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Perigee

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Inclination

43.00°

Right Ascension

356.58°

Eccentricity

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Argument of Perigee

231.94°

Period

91.66 min

Mean Motion

15.71 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-11510 [DTC]

Alternative Name

Starlink 11510

Type

Payload

Status

Operational

Owner

SPXS

Country

United States

Constellation

N/A

Related Satellites

Major Events

N/A

Latest TLEs
1 62516U 25004F   26200.48585147  .00144862  00000+0  11072-2 0  9990
2 62516  43.0034 356.5758 0002022 231.9417 128.1269 15.70962199 87933

Source: Celestrak

Summary
The STARLINK-11510 [DTC], also known as Starlink 11510, is a Starlink V2M satellite owned by SPXS and launched on January 8, 2025, from LC39A at AFETR using a Falcon 9 launch vehicle. It has dimensions of approximately 0.3 meters in length, 4.1 meters in diameter, and a span of 29 meters. The satellite's dry mass is 700 kg, with a launch mass of 730 kg. Its shape consists of a box structure with solar panels. The satellite was part of the Starlink Group 12-11-06 payload and operates in a constellation for unspecified purposes.

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 12-11-06

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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