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Astranis UtilitySat (62454)
COSPAR: 2024-252A | Alt Name: UtilitySat
Image
Additional Sources
Launch Details
Launch Date
December 29, 2024
Launch Site
Cape Canaveral Space Force Station
Launch Pad
SLC-40
Launch Vehicle
Orbital Elements
NORAD ID
62454
International Designator
2024-252A
Epoch
Thu, 16 Jul 2026 23:53:35 GMT
Apogee
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Perigee
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Inclination
9.14°
Right Ascension
326.33°
Eccentricity
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Argument of Perigee
256.75°
Period
1435.87 min
Mean Motion
1.00 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
Astranis UtilitySat
Alternative Name
UtilitySat
Type
Payload
Status
Operational
Owner
Astranis
Country
United States
Constellation
N/A
Related Satellites
Major Events
Launched on December 29, 2024, aboard a Falcon 9 rocket; designed for multiple relocations to serve various missions.
Latest TLEs
1 62454U 24252A 26197.99554528 -.00000142 00000+0 00000+0 0 9994
2 62454 9.1369 326.3258 7536513 256.7459 17.9070 01.00287842 5728
Source: Celestrak
Summary
The Astranis UtilitySat (NORAD_CAT_ID: 62454) is a MicroGEO configuration satellite owned and manufactured by Astranis for providing flexible broadband connectivity. Launched on December 29, 2024, from Cape Canaveral Space Force Station's SLC-40 pad using a Falcon 9 rocket, the UtilitySat has dimensions of 1.5 meters in length and diameter with a span of 10 meters when solar panels are deployed. It weighs 400 kg at launch and is designed for multiple relocations within the geostationary belt over its operational life. The satellite is equipped with a proprietary ultra-wideband software-defined radio that supports Ku, Ka, and Q/V bands, enabling flexible frequency allocation. Power comes from solar arrays with onboard battery storage, while propulsion includes both a chemical monopropellant system and an electric ion thruster. The UtilitySat's structure consists of aluminum and composite materials, with a silver color finish. Its mission focuses on offering versatile broadband services for disaster relief, capacity bridge needs, and surge requirements.
Physical Characteristics
Length
1.5
Diameter
1.5
Span
10
Dry Mass
400
Launch Mass
400
Shape
Box with deployable solar panels
Radar Cross Section
0.122
Visual Magnitude
5
Color
Silver
Material Composition
Aluminum and composite materials
Technical Details
Payload
Astranis Block 2-1
Purpose
Unknown
Mission
To provide flexible, on-demand broadband connectivity for various applications, including disaster relief, bridge capacity, and surge needs.
Manufacturer
Astranis
Life Expectancy
Designed for multiple relocations within the geostationary belt over its operational life.
Bus
MicroGEO
Configuration
UtilitySat
Motor
Dual-propulsion system comprising a chemical monopropellant system and an electric ion thruster.
Equipment
Equipped with a proprietary ultra-wideband software-defined radio, enabling flexible frequency allocation across Ku, Ka, and Q/V bands.
Power System
Powered by solar arrays, with energy storage in onboard batteries.
ADCS
Unknown
Transmitter Frequency
Ku, Ka, and Q/V bands
Map
Next Pass
Azimuth Elevation Time (Local)
Start Azimuth
Max Elevation
Stop Azimuth
Time Until
Pass Duration
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