BIRKELAND, 55015
Orbit data source: Space-Track
BIRKELAND, 55015 is a Norwegian payload satellite in SSO that was launched on Tue, 03 Jan 2023 UTC via an FALCON 9 launch vehicle from the Air Force Eastern Test Range (AFETR). 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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55015 intel report (Beta)
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Identifier
Orbit
Country
NO / NORRelated business
Manufacturer
NanoAvionics
Mission
Operational Civil Sigint
Bus & Motor
CUBESAT 6U, Unknown motor
Mass
10 kg wet, ~10 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Box + 2 Pan, 0.1 m
Radar Cross Section
0.080 m², Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 7 hours ago
TLE from 7 hours ago
0 BIRKELAND
1 55015U 23001G 26068.80731652 .00010710 00000-0 28651-3 0 9990
2 55015 97.3442 136.6128 0008690 103.4677 256.7537 15.38190524177069Epoch: 2026-03-09T19:22Z
TLE epoch observation values (Epoch: 2026-03-09T19:22:32.147Z)
Latitude
-0.00002°
Longitude
38.48389°
Altitude
455.942 km
Speed
7.638 km/s
True Right ascension
09h 06m 27s
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
06:35:55
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
454.331 km
Perigee altitude
442.467 km
Semi-major axis
6,826.536 km
Eccentricity
0.00087
Inclination
97.3442°
RAAN
136.6128°
Arg. of periapsis
103.4677°
True anomaly
256.65679°
Mean anomaly
256.7537°
Eccentric anomaly
256.70524°
Mean motion
3.84807 °/min
Orbital period
93.55 mins
BSTAR
0.00028651
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Other satellites on launch #1 in the year 2023 (2023-01-03 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.BIRKELAND 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. |
|---|---|---|---|---|---|---|---|
| 4 mins | 2026-03-10 04:53:15.196Z | 205.656° SW | 2026-03-10 04:55:15.196Z | 281.423° WNW | 31.714° | 2026-03-10 04:57:15.196Z | 327.056° NNW |
| 4 mins | 2026-03-10 17:48:15.196Z | 337.752° N | 2026-03-10 17:50:15.196Z | 273.547° WNW | 28.415° | 2026-03-10 17:52:15.196Z | 227.359° WSW |
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 descending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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