STARLINK-2363 (47903)

COSPAR: 2021-021AV | Alt Name: Starlink 2363

Image
STARLINK-2363 Satellite Image
Additional Sources
Launch Details

Launch Date

March 14, 2021

Launch Pad

LC39A

Launch Vehicle

Falcon 9

Orbital Elements

NORAD ID

47903

International Designator

2021-021AV

Epoch

Sat, 04 Jul 2026 00:58:39 GMT

Apogee

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Perigee

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Inclination

53.14°

Right Ascension

29.98°

Eccentricity

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Argument of Perigee

272.73°

Period

89.14 min

Mean Motion

16.15 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-2363

Alternative Name

Starlink 2363

Type

Payload

Status

Operational

Owner

SPXS

Country

United States

Constellation

N/A

Related Satellites

Major Events

N/A

Latest TLEs
1 47903U 21021AV  26185.04073450  .01319340  12980-2  94668-3 0  9993
2 47903  53.1417  29.9754 0013005 272.7276  87.2272 16.15406823295206

Source: Celestrak

Summary
STARLINK-2363 is a communication satellite operated by SpaceX (SPXS), designated under the Starlink program. Launched on March 14, 2021, from Launch Complex 39A at Kennedy Space Center using a Falcon 9 launch vehicle, this satellite has a length of 0.2 meters, a diameter of 2.8 meters, and a span of 9 meters. It has a dry mass of 248 kg and a launch mass of 260 kg. Equipped with Ku/Ka-band payload and optical inter-satellite links (prototypes), the satellite is powered by solar arrays and batteries and uses krypton ion thrusters for propulsion. The shape of the satellite is described as "Box + pan."

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

248

Launch Mass

260

Shape

Box + pan

Radar Cross Section

Unknown

Visual Magnitude

Unknown

Color

Unknown

Material Composition

Unknown

Technical Details

Payload

Starlink V1.0-L21-44

Purpose

Communication

Mission

Communication

Manufacturer

SPXS

Life Expectancy

Unknown

Bus

Starlink

Configuration

Unknown

Motor

Krypton ion thrusters

Equipment

Ku/Ka-band payload (all), optical inter-satellite links (a few prototypes)

Power System

Solar arrays, batteries

ADCS

Unknown

Transmitter Frequency

Unknown

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