STARLINK-31649 (59390)

COSPAR: 2024-062S | Alt Name: Starlink 31649

Image
STARLINK-31649 Satellite Image
Additional Sources
Launch Details

Launch Date

April 2, 2024

Launch Site

AFWTR

Launch Pad

SLC4E

Launch Vehicle

Falcon 9

Orbital Elements

NORAD ID

59390

International Designator

2024-062S

Epoch

Sun, 19 Jul 2026 20:12:37 GMT

Apogee

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Perigee

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Inclination

53.16°

Right Ascension

0.48°

Eccentricity

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Argument of Perigee

95.05°

Period

93.85 min

Mean Motion

15.34 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-31649

Alternative Name

Starlink 31649

Type

Payload

Status

Operational

Owner

SPXS

Country

United States

Constellation

N/A

Related Satellites

Major Events

N/A

Latest TLEs
1 59390U 24062S   26200.84209962 -.00000930  00000+0 -16383-4 0  9998
2 59390  53.1585   0.4783 0001440  95.0462 265.0705 15.34388345129924

Source: Celestrak

Summary
STARLINK-31649 is a Starlink v2 Mini satellite (NORAD_CAT_ID: 59390) launched on April 2, 2024, from AFWTR SLC4E using the Falcon 9 launch vehicle. It has dimensions of 0.3 meters in length and 4.1 meters in diameter with a span of 29 meters. The satellite weighs 700 kilograms dry and 730 kilograms at launch. Equipped with Ku/Ka/E-band payload and optical inter-satellite link, it is designed for communication purposes and uses Argon ion thrusters as propulsion and solar arrays with batteries for power. It was manufactured by SPXS and is part of the Starlink Group 7-18-17 mission under ownership of SpaceX (SPXS).

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

0.3

Diameter

4.1

Span

29

Dry Mass

700

Launch Mass

730

Shape

Box + pan

Radar Cross Section

Unknown

Visual Magnitude

Unknown

Color

Unknown

Material Composition

Unknown

Technical Details

Payload

Starlink Group 7-18-17

Purpose

Communication

Mission

Communication

Manufacturer

SPXS

Life Expectancy

Unknown

Bus

Starlink V2M

Configuration

Starlink v2 Mini

Motor

Argon ion thrusters

Equipment

Ku/Ka/E-band payload, optical inter-satellite link

Power System

Solar arrays, batteries

ADCS

Unknown

Transmitter Frequency

Unknown

Map
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