ASBM-2, 60423
Orbit data source: Space-Track
ASBM-2, 60423 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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60423 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
3,505 kg wet, 1,925 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: 1 week ago
TLE from 1 week ago
0 ASBM-2
1 60423U 24143B 25251.96432912 -.00000002 00000-0 00000-0 0 9993
2 60423 62.5998 56.4143 5483627 268.7398 31.2939 1.50425493 7363Epoch: 2025-09-08T23:08Z
TLE epoch observation values (Epoch: 2025-09-08T23:08:38.035Z)
Latitude
0.00004°
Longitude
80.93642°
Altitude
16,363.325 km
Speed
4.761 km/s
True Right ascension
03h 45m 25s
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
14:01:19
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
43,440.069 km
Perigee altitude
8,153.187 km
Semi-major axis
32,174.765 km
Eccentricity
0.54836
Inclination
62.5998°
RAAN
56.4143°
Arg. of periapsis
268.7398°
True anomaly
91.38765°
Mean anomaly
31.2939°
Eccentric anomaly
57.91342°
Mean motion
0.37607 °/min
Orbital period
957.27 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-2 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. |
|---|---|---|---|---|---|---|---|
| 358 mins | 2025-09-15 21:21:27.212Z | 323.117° NNW | 2025-09-15 22:56:27.212Z | 319.645° NNW | 33.359° | 2025-09-16 03:19:27.212Z | 273.606° WNW |
| 782 mins | 2025-09-16 06:59:27.212Z | 97.299° ESE | 2025-09-16 11:31:27.212Z | 41.755° NE | 36.186° | 2025-09-16 20:01:27.212Z | 124.128° SE |
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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