STARLINK-32778 (62603)

COSPAR: 2025-008S | Alt Name: Starlink 32778

Image
STARLINK-32778 Satellite Image
Additional Sources
Launch Details

Launch Date

January 13, 2025

Launch Pad

LC40

Launch Vehicle

Falcon 9

Orbital Elements

NORAD ID

62603

International Designator

2025-008S

Epoch

Sun, 19 Jul 2026 05:07:08 GMT

Apogee

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Perigee

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Inclination

43.00°

Right Ascension

255.63°

Eccentricity

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Argument of Perigee

212.30°

Period

94.27 min

Mean Motion

15.28 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-32778

Alternative Name

Starlink 32778

Type

Payload

Status

Operational

Owner

SPXS

Country

United States

Constellation

N/A

Related Satellites

Major Events

N/A

Latest TLEs
1 62603U 25008S   26200.21328929  .00010982  00000+0  40770-3 0  9998
2 62603  42.9979 255.6285 0001478 212.2967 147.7795 15.27605207 85672

Source: Celestrak

Summary
The satellite named STARLINK-32778 (OBJECT_ID: 2025-008S) is a Starlink V2M model belonging to SpaceX (SPXS). Launched on January 13, 2025, from LC40 at AFETR using a Falcon 9 launch vehicle, the satellite has dimensions of 0.3 meters in length, a diameter of 4.1 meters, and spans 29 meters when deployed. It weighs 730 kg at launch with a dry mass of 700 kg. The shape is described as "Box + pan," indicating its design features both box-like and panel components. The satellite is part of the Starlink Group 12-4-17 payload, though specific mission details are not provided in the data.

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 12-4-17

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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