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STARLINK-30863 (59027)
COSPAR: 2024-038E | Alt Name: Starlink 30863
Image
Additional Sources
Launch Details
Launch Date
February 25, 2024
Launch Site
Launch Pad
LC40
Launch Vehicle
Orbital Elements
NORAD ID
59027
International Designator
2024-038E
Epoch
Sun, 19 Jul 2026 20:10:39 GMT
Apogee
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Perigee
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Inclination
43.00°
Right Ascension
1.14°
Eccentricity
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Argument of Perigee
274.69°
Period
94.27 min
Mean Motion
15.28 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
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Basic Satellite Info
Name
STARLINK-30863
Alternative Name
Starlink 30863
Type
Payload
Status
Operational
Owner
SPXS
Country
United States
Constellation
N/A
Related Satellites
Major Events
N/A
Latest TLEs
1 59027U 24038E 26200.84074052 -.00006729 00000+0 -23502-3 0 9990
2 59027 43.0039 1.1443 0001507 274.6939 85.3741 15.27605195134850
Source: Celestrak
Summary
The Starlink V2M satellite identified by NORAD_CAT_ID 59027 and OBJECT_ID 2024-038E is a Starlink v2 Mini model, manufactured by SPXS (SpaceX). It was launched on February 25, 2024, from Launch Pad LC40 at the AFETR site using a Falcon 9 launch vehicle. The satellite has dimensions of 0.3 meters in length and 4.1 meters in diameter with a span of 29 meters. Its dry mass is 700 kg, and it has a launch mass of 730 kg. It is equipped with Ku/Ka/E-band payload and optical inter-satellite link for communication purposes, powered by solar arrays and batteries. The satellite's propulsion system includes Argon ion thrusters and its shape consists of a box structure with panels.
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 6-39-05
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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