STARLINK-5502 (55644)

COSPAR: 2023-021S | Alt Name: Starlink 5502

Image
STARLINK-5502 Satellite Image
Additional Sources
Launch Details

Launch Date

February 17, 2023

Launch Site

AFWTR

Launch Pad

SLC4E

Launch Vehicle

Falcon 9

Orbital Elements

NORAD ID

55644

International Designator

2023-021S

Epoch

Sun, 19 Jul 2026 18:23:02 GMT

Apogee

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Perigee

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Inclination

70.00°

Right Ascension

211.50°

Eccentricity

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Argument of Perigee

266.78°

Period

96.11 min

Mean Motion

14.98 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-5502

Alternative Name

Starlink 5502

Type

Payload

Status

Operational

Owner

SPXS

Country

United States

Constellation

N/A

Related Satellites

Major Events

N/A

Latest TLEs
1 55644U 23021S   26200.76600676  .00000269  00000+0  30353-4 0  9994
2 55644  69.9993 211.5013 0003505 266.7841  93.2917 14.98331628188576

Source: Celestrak

Summary
The STARLINK-5502 satellite, also known as Starlink 5502, is a communication satellite manufactured by SPXS (SpaceX) and launched on February 17, 2023, from AFWTR using the Falcon 9 launch vehicle at SLC4E. The spacecraft has dimensions of 0.2 meters in length, 2.8 meters in diameter, and spans 9 meters. It weighs 305 kilograms at launch with a dry mass of 290 kilograms. Equipped with Ku/Ka-band payload and an optical inter-satellite link for communication purposes, it uses krypton ion thrusters as its propulsion system and is powered by solar arrays and batteries. The satellite's shape is described as box-shaped with a pan configuration and falls under the Starlink Group 2-5-17 mission.

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

290

Launch Mass

305

Shape

Box + pan

Radar Cross Section

Unknown

Visual Magnitude

Unknown

Color

Unknown

Material Composition

Unknown

Technical Details

Payload

Starlink Group 2-5-17

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

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