STARLINK-1669 (47624)

COSPAR: 2021-012E | Alt Name: Starlink 1669

Image
STARLINK-1669 Satellite Image
Additional Sources
Launch Details

Launch Date

February 16, 2021

Launch Pad

LC40

Launch Vehicle

Falcon 9

Orbital Elements

NORAD ID

47624

International Designator

2021-012E

Epoch

Fri, 24 Apr 2026 21:28:01 GMT

Apogee

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Perigee

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Inclination

53.01°

Right Ascension

115.64°

Eccentricity

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Argument of Perigee

283.16°

Period

87.51 min

Mean Motion

16.46 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-1669

Alternative Name

Starlink 1669

Type

Payload

Status

Partially operational

Owner

SPXS

Country

United States

Constellation

N/A

Related Satellites

Major Events

N/A

Latest TLEs
1 47624U 21012E   26114.89445721  .13358059  12536-4  35260-3 0  9997
2 47624  53.0100 115.6370 0004488 283.1636  76.8911 16.45576092288487

Source: Celestrak

Summary
STARLINK-1669, also known as Starlink 1669, is a communication satellite operated by SPXS (SpaceX). Launched on February 16, 2021, from LC40 at AFETR using the Falcon 9 launch vehicle, it has a BUS type of Starlink. The satellite measures 0.2 meters in length with a diameter of 2.8 meters and a span of 9 meters. It has a dry mass of 248 kg and was launched with a total mass of 260 kg. Equipped with Ku/Ka-band payload (all) and optical inter-satellite links (a few prototypes), it uses solar arrays and batteries for power and employs krypton ion thrusters for propulsion. Its shape is described as "Box + pan" and its purpose is to provide communication services.

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-L19-05

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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