ASBM-1, 60422
Orbit data source: Space-Track
ASBM-1, 60422 is a Norwegian payload satellite in HEO that was launched on Mon, 12 Aug 2024 UTC via an FALCON 9 launch vehicle from the Air Force Western Test Range (AFWTR). Payload-class satellites include a variety of spacecraft equipped with specific instruments for various scientific and technological missions. These include communications satellites like Starlink; space stations such as the ISS; scientific satellites like the Hubble; Earth observation satellites from companies like Planet Labs, Umbra, and HawkEye 360; GPS; miniature CubeSats for education and research; and military/defense satellites.
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60422 intel report (Beta)
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Edit Public Description
Identifier
Orbit
Country
NO / NORRelated business
Manufacturer
NGIS SSG
Mission
Operational Commercial Communications
Bus & Motor
GEOSTAR-3, BT-4?
Mass
3,695 kg wet, 2,035 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Box + 2 Pan, 13.5 m
Radar Cross Section
35.796 m², Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 3 weeks ago
TLE from 3 weeks ago
0 ASBM-1
1 60422U 24143A 25243.65418871 -.00000049 00000-0 00000-0 0 9998
2 60422 62.6373 56.6611 5481566 268.7204 31.2902 1.50427878 7266Epoch: 2025-08-31T15:42Z
TLE epoch observation values (Epoch: 2025-08-31T15:42:01.904Z)
Latitude
-0.0001°
Longitude
-158.94285°
Altitude
16,379.77 km
Speed
4.758 km/s
True Right ascension
03h 46m 32s
True Declination
0° 00' 00"
Sunlit
Visualization orbit readout
Latitude
Unknown
Longitude
Unknown
Altitude
Unknown
Speed
Unknown
Apparent Right ascension
Unknown
Apparent Declination
Unknown
Sunlit
Visualization observer readout
Local Sidereal Time
07:32:49
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
43,432.909 km
Perigee altitude
8,159.664 km
Semi-major axis
32,174.423 km
Eccentricity
0.54816
Inclination
62.6373°
RAAN
56.6611°
Arg. of periapsis
268.7204°
True anomaly
91.34795°
Mean anomaly
31.2902°
Eccentric anomaly
57.89409°
Mean motion
0.37608 °/min
Orbital period
957.25 mins
BSTAR
0
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Other satellites on launch #143 in the year 2024 (2024-08-12 UTC)
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You can import UDL-sourced sensor .json files into the Sandbox to generate a visibility chart that accounts for multi-vendor sensor geometry.ASBM-1 Visibility forecast
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Span | Click to sort rows by Start time (UTC) header in descending order | Start Az. | Max El. time (UTC) | Max El. Az. | Max El. | End time (UTC) | End Az. |
|---|---|---|---|---|---|---|---|
| 745 mins | 2025-09-18 14:42:12.517Z | 250.602° W | 2025-09-18 22:44:12.517Z | 319.612° NNW | 33.426° | 2025-09-19 03:07:12.517Z | 273.203° WNW |
| 475 mins | 2025-09-19 06:47:12.517Z | 96.768° ESE | 2025-09-19 11:18:12.517Z | 41.689° NE | 36.136° | 2025-09-19 14:42:12.517Z | 40.365° NE |
Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
Click to sort rows by RSO header in ascending order | Click to sort rows by Country header in ascending order | Click to sort rows by Type header in ascending order | Click to sort rows by Inclination Δ header in ascending order | Click to sort rows by RAAN Δ header in ascending order | Click to sort rows by Coplanar Angle header in ascending order | Click to sort rows by SMA Δ header in ascending order | Click to sort rows by Orbital period header in ascending order | Click to sort rows by <5km Md TCA header in ascending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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Click to sort rows by Secondary header in ascending order | Click to sort rows by Secondary name header in ascending order | Click to sort rows by Country header in ascending order | Click to sort rows by Owner header in ascending order | Click to sort rows by Obj. Type header in ascending order | Click to sort rows by Miss dist. header in ascending order | Click to sort rows by Rel. speed header in ascending order | Click to sort rows by Apr. angle header in ascending order | Click to sort rows by TCA header in ascending order |
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