STARLINK-3648 (51993)

COSPAR: 2022-025AP | Alt Name: Starlink 3648

Image
STARLINK-3648 Satellite Image
Additional Sources
Launch Details

Launch Date

March 9, 2022

Launch Pad

LC40

Launch Vehicle

Falcon 9

Orbital Elements

NORAD ID

51993

International Designator

2022-025AP

Epoch

Mon, 20 Jul 2026 02:33:23 GMT

Apogee

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Perigee

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Inclination

53.16°

Right Ascension

164.38°

Eccentricity

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Argument of Perigee

88.55°

Period

95.44 min

Mean Motion

15.09 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-3648

Alternative Name

Starlink 3648

Type

Payload

Status

Operational

Owner

SPXS

Country

United States

Constellation

N/A

Related Satellites

Major Events

N/A

Latest TLEs
1 51993U 22025AP  26201.10651994  .00000392  00000+0  42747-4 0  9995
2 51993  53.1611 164.3827 0001228  88.5517 271.5615 15.08836948241055

Source: Celestrak

Summary
The STARLINK-3648 satellite, also known as Starlink 3648, is operated by SPXS and serves a communication mission under the Starlink Group 4-10-38 payload. It was launched on March 9, 2022, from Launch Pad LC40 at AFETR using a Falcon 9 launch vehicle. The satellite has dimensions of 0.2 meters in length, a diameter of 2.8 meters, and a span of 9 meters. Its dry mass is recorded as 275 kilograms, with a total launch mass of 297 kilograms. It features a Ku/Ka-band payload along with an optical inter-satellite link for communication purposes. The spacecraft employs krypton ion thrusters for propulsion and is powered by solar arrays and batteries. Its structure can be described as having a box shape with an additional pan configuration.

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

0.2

Diameter

2.8

Span

9

Dry Mass

275

Launch Mass

297

Shape

Box + pan

Radar Cross Section

Unknown

Visual Magnitude

Unknown

Color

Unknown

Material Composition

Unknown

Technical Details

Payload

Starlink Group 4-10-38

Purpose

Communication

Mission

Communication

Manufacturer

SPXS

Life Expectancy

Unknown

Bus

Starlink

Configuration

Unknown

Motor

Krypton ion thrusters

Equipment

Ku/Ka-band payload, optical inter-satellite link

Power System

Solar arrays, batteries

ADCS

Unknown

Transmitter Frequency

Unknown

Map
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