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ASBM-1 (60422)
COSPAR: 2024-143A | Alt Name: GX10A
Image
Additional Sources
Launch Details
Launch Date
August 11, 2024
Launch Site
Vandenberg Space Force Base, California
Launch Pad
SLC-4E
Launch Vehicle
Orbital Elements
NORAD ID
60422
International Designator
2024-143A
Epoch
Thu, 02 Jul 2026 18:51:56 GMT
Apogee
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Perigee
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Inclination
62.87°
Right Ascension
44.86°
Eccentricity
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Argument of Perigee
269.34°
Period
957.28 min
Mean Motion
1.50 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
ASBM-1
Alternative Name
GX10A
Type
Payload
Status
Operational
Owner
Space Norway HEOSAT
Country
NO
Constellation
Arctic Satellite Broadband Mission
Related Satellites
Major Events
Launch on August 11, 2024; expected operational service in early to mid-2025
Latest TLEs
1 60422U 24143A 26183.78607562 -.00000090 00000+0 00000+0 0 9997
2 60422 62.8694 44.8641 5614464 269.3377 29.5572 01.50426492 11853
Source: Celestrak
Summary
ASBM-1 (GX10A) is a satellite operated by Space Norway HEOSAT and manufactured by Northrop Grumman using the GEOStar-3 Bus configuration. Launched on August 11, 2024, from Vandenberg Space Force Base's SLC-4E pad aboard a Falcon 9 launch vehicle, it aims to provide continuous broadband coverage for both civilian and military communications in the Arctic region under the Arctic Satellite Broadband Mission (ASBM). The satellite is equipped with Ka-band transponders for Viasat, X-band transponders for the Norwegian Armed Forces, EHF payload for the U.S. Space Force, and a Norwegian Radiation Monitor (NORM). With dimensions of 4 meters in length, 3 meters in diameter, and a span of 27 meters due to its solar panel wings, ASBM-1 has an operational lifetime of 15 years and was launched with a mass of 3695 kg. It is powered by two deployable solar arrays that provide 7,235 W end-of-life power and batteries with a capacity of 9,910 Wh. The satellite's dry mass is 2035 kg and it uses bi-propellant for orbital maneuvers and monopropellant for stationkeeping. It features 3-axis stabilization and has an aluminum and composite materials composition, appearing silver in color. Its major events include launch on August 11, 2024, with expected operational service starting early to mid-2025.
Physical Characteristics
Length
4
Diameter
3
Span
27
Dry Mass
2035
Launch Mass
3695
Shape
Box with two solar panel wings
Radar Cross Section
Unknown
Visual Magnitude
Unknown
Color
Silver
Material Composition
Aluminum and composite materials
Technical Details
Payload
Ka-band payload for Viasat, X-band payload for the Norwegian Armed Forces, EHF payload for the U.S. Space Force, Norwegian Radiation Monitor (NORM)
Purpose
Communication
Mission
The Arctic Satellite Broadband Mission (ASBM) aims to provide continuous broadband coverage to the Arctic region, supporting both civilian and military communications.
Manufacturer
Northrop Grumman
Life Expectancy
15 years
Bus
GEOStar-3
Configuration
GEOStar-3 Bus
Motor
Bi-propellant for orbital maneuvers; monopropellant for stationkeeping
Equipment
Ka-band transponders, X-band transponders, EHF payload, Norwegian Radiation Monitor (NORM)
Power System
Two deployable solar arrays providing 7,235 W end-of-life power; batteries with 9,910 Wh capacity
ADCS
3-axis stabilized
Transmitter Frequency
Ka-band, X-band, EHF
Map
Next Pass
Azimuth Elevation Time (Local)
Start Azimuth
Max Elevation
Stop Azimuth
Time Until
Pass Duration
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