STARLINK-5303 (55630)

COSPAR: 2023-021C | Alt Name: Starlink 5303

Image
STARLINK-5303 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

55630

International Designator

2023-021C

Epoch

Sun, 19 Jul 2026 18:53:24 GMT

Apogee

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Perigee

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Inclination

70.00°

Right Ascension

231.45°

Eccentricity

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Argument of Perigee

269.46°

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-5303

Alternative Name

Starlink 5303

Type

Payload

Status

Operational

Owner

SPXS

Country

United States

Constellation

N/A

Related Satellites

Major Events

N/A

Latest TLEs
1 55630U 23021C   26200.78708867 -.00000159  00000+0 -55445-5 0  9992
2 55630  69.9986 231.4473 0003527 269.4579  90.6176 14.98330774188081

Source: Celestrak

Summary
STARLINK-5303 is a communication satellite belonging to the Starlink constellation, launched by SpaceX (SPXS) on February 17, 2023, from AFWTR SLC4E using a Falcon 9 launch vehicle. The satellite has dimensions of 0.2 meters in length and 2.8 meters in diameter, with an overall span of 9 meters. It weighs approximately 290 kilograms dry and had a launch mass of 305 kilograms. Equipped with Ku/Ka-band payload capabilities and optical inter-satellite link technology, it uses solar arrays and batteries for power supply and employs krypton ion thrusters as its motor system. The satellite's shape is described as a box with a panel 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

290

Launch Mass

305

Shape

Box + pan

Radar Cross Section

Unknown

Visual Magnitude

Unknown

Color

Unknown

Material Composition

Unknown

Technical Details

Payload

Starlink Group 2-5-03

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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