STARLINK-1983 (47630)

COSPAR: 2021-012L | Alt Name: Starlink 1983

Image
STARLINK-1983 Satellite Image
Additional Sources
Launch Details

Launch Date

February 16, 2021

Launch Pad

LC40

Launch Vehicle

Falcon 9

Orbital Elements

NORAD ID

47630

International Designator

2021-012L

Epoch

Fri, 03 Jul 2026 20:13:05 GMT

Apogee

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Perigee

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Inclination

53.16°

Right Ascension

229.16°

Eccentricity

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Argument of Perigee

80.14°

Period

94.01 min

Mean Motion

15.32 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-1983

Alternative Name

Starlink 1983

Type

Payload

Status

Operational

Owner

SPXS

Country

United States

Constellation

N/A

Related Satellites

Major Events

N/A

Latest TLEs
1 47630U 21012L   26184.84242678  .00001417  00000-0  57408-4 0  9999
2 47630  53.1565 229.1587 0001259  80.1436 279.9708 15.31708377298070

Source: Celestrak

Summary
The STARLINK-1983 satellite, also known as Starlink 1983, is operated by SpaceX (SPXS). It was launched on February 16, 2021, from the Cape Canaveral Space Force Station Launch Complex 40 using a Falcon 9 launch vehicle. The spacecraft has dimensions of 0.2 meters in length, 2.8 meters in diameter, and spans 9 meters. With a dry mass of 248 kg and a launch mass of 260 kg, it is equipped with a Ku/Ka-band payload (all) and optical inter-satellite links (for prototypes). The satellite is powered by solar arrays and batteries and uses krypton ion thrusters for propulsion. Its mission is focused on communication purposes as part of the Starlink constellation.

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-L19-11

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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