X Report 13 Mar 2025
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STARLINK-31886 (59662)
COSPAR: 2024-084J | Alt Name: Starlink 31886
Image
Additional Sources
Launch Details
Launch Date
May 6, 2024
Launch Site
Launch Pad
LC40
Launch Vehicle
Orbital Elements
NORAD ID
59662
International Designator
2024-084J
Epoch
Sun, 19 Jul 2026 20:24:40 GMT
Apogee
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Perigee
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Inclination
43.00°
Right Ascension
15.58°
Eccentricity
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Argument of Perigee
268.87°
Period
94.27 min
Mean Motion
15.28 rev/day
Latitude
Calculating...
Longitude
Calculating...
Altitude
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Velocity
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Polar Plot
3D Visualization
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Basic Satellite Info
Name
STARLINK-31886
Alternative Name
Starlink 31886
Type
Payload
Status
Operational
Owner
SPXS
Country
United States
Constellation
N/A
Related Satellites
Major Events
N/A
Latest TLEs
1 59662U 24084J 26200.85046462 -.00000706 00000+0 -16158-4 0 9990
2 59662 43.0021 15.5799 0001043 268.8702 91.2030 15.27571271124580
Source: Celestrak
Summary
The Starlink V2M satellite, designated STARLINK-31886 or Starlink 31886, was launched on May 6, 2024, from Cape Canaveral Air Force Station's Launch Complex 40 using a Falcon 9 launch vehicle. This communication satellite has dimensions of 0.3 meters in length and 4.1 meters in diameter with a span of 29 meters. It is equipped with Ku/Ka/E-band payload capabilities along with an optical inter-satellite link, solar arrays for power generation, and batteries. The satellite weighs 730 kilograms at launch and has a dry mass of 700 kilograms. Its propulsion system consists of Argon ion thrusters. Manufactured by SpaceX (SPXS), the Starlink V2M is part of the Starlink Group 6-57-09 payload, aimed to enhance global 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.
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 6-57-09
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
Next Pass
Azimuth Elevation Time (Local)
Start Azimuth
Max Elevation
Stop Azimuth
Time Until
Pass Duration
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