STARLINK-11516 [DTC] (62522)

COSPAR: 2025-004M | Alt Name: Starlink 11516

Image
STARLINK-11516 [DTC] Satellite Image
Additional Sources
Launch Details

Launch Date

January 8, 2025

Launch Pad

LC39A

Launch Vehicle

Falcon 9

Orbital Elements

NORAD ID

62522

International Designator

2025-004M

Epoch

Sun, 19 Jul 2026 18:39:12 GMT

Apogee

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Perigee

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Inclination

43.00°

Right Ascension

354.44°

Eccentricity

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Argument of Perigee

284.55°

Period

91.67 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-11516 [DTC]

Alternative Name

Starlink 11516

Type

Payload

Status

Operational

Owner

SPXS

Country

United States

Constellation

N/A

Related Satellites

Major Events

N/A

Latest TLEs
1 62522U 25004M   26200.77722484  .00165414  00000+0  12659-2 0  9994
2 62522  43.0002 354.4417 0001401 284.5456  75.5256 15.70863081 87987

Source: Celestrak

Summary
The satellite named STARLINK-11516 [DTC], also known as Starlink 11516, is a part of the Starlink V2M series launched by SpaceX (SPXS) on January 8, 2025, from LC39A at AFETR using a Falcon 9 launch vehicle. It has dimensions of 0.3 meters in length and a diameter of 4.1 meters with a span of 29 meters. The satellite's dry mass is 700 kilograms while its launch mass was 730 kilograms. Its shape is described as "Box + pan". This satellite is part of the Starlink Group 12-11-12 payload, owned by SpaceX and operating under US jurisdiction.

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 12-11-12

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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