STARLINK-33575 (62760)

COSPAR: 2025-015C | Alt Name: Starlink 33575

Image
STARLINK-33575 Satellite Image
Additional Sources
Launch Details

Launch Date

January 21, 2025

Launch Site

AFWTR

Launch Pad

SLC4E

Launch Vehicle

Falcon 9

Orbital Elements

NORAD ID

62760

International Designator

2025-015C

Epoch

Mon, 20 Jul 2026 00:46:23 GMT

Apogee

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Perigee

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Inclination

53.16°

Right Ascension

65.57°

Eccentricity

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Argument of Perigee

90.94°

Period

93.85 min

Mean Motion

15.34 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-33575

Alternative Name

Starlink 33575

Type

Payload

Status

Operational

Owner

SPXS

Country

United States

Constellation

N/A

Related Satellites

Major Events

N/A

Latest TLEs
1 62760U 25015C   26201.03221321  .00011714  00000+0  35726-3 0  9998
2 62760  53.1584  65.5665 0001155  90.9397 269.1738 15.34401909 84016

Source: Celestrak

Summary
The STARLINK-33575 satellite, also known as Starlink 33575, is a component of the Starlink V2MO series launched on January 21, 2025, from Space Launch Complex 4E at Vandenberg Air Force Base using a Falcon 9 launch vehicle. The spacecraft has dimensions of 0.3 meters in length and 4.1 meters in diameter with a span of 29 meters. It was manufactured by SpaceX (SPXS) and had a dry mass of 530 kilograms, with an initial launch mass of 575 kilograms. The satellite is part of the Starlink Group 11-8-03 payload and has a shape described as "Box + pan." Ownership is attributed to SpaceX.

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

530

Launch Mass

575

Shape

Box + pan

Radar Cross Section

Unknown

Visual Magnitude

Unknown

Color

Unknown

Material Composition

Unknown

Technical Details

Payload

Starlink Group 11-8-03

Purpose

Unknown

Mission

Unknown

Manufacturer

SPXS

Life Expectancy

Unknown

Bus

Starlink V2MO

Configuration

Unknown

Motor

Unknown

Equipment

Unknown

Power System

Unknown

ADCS

Unknown

Transmitter Frequency

Unknown

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