Showing default

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.

Loading next visibility...
Identifier
55015, 2023-001G
Orbit
SSO
Country
Flag of NONO / NOR
Related business
Manufacturer
NanoAvionics
Mission
Operational Civil Sigint
Bus & Motor
CUBESAT 6U, Unknown motor
Mass
10 kg wet, ~10 kg dry
Launch date (UTC)
2023-01-03 (3 years ago)
Launch vehicle
FALCON 9
Launch site
Air Force Eastern Test Range (AFETR)
Object type
Payload
Rocket body
Debris
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 & history
Last TLE update: 19 hours ago

TLE from 19 hours ago
0 BIRKELAND
1 55015U 23001G   26022.92801601  .00011794  00000-0  32704-3 0  9992
2 55015  97.3536  90.6966 0005547 265.4070  94.6541 15.37075384170013
Epoch: 2026-01-22T22:16Z
TLE epoch observation values (Epoch: 2026-01-22T22:16:20.583Z)
Latitude
-0.00001°
Longitude
-5.66331°
Altitude
458.188 km
Speed
7.638 km/s
True Right ascension
06h 02m 47s
True Declination
0° 00' 00"
Sunlit
Object was in full shadow at epoch
Visualization orbit readout
Latitude
Unknown
Longitude
Unknown
Altitude
Unknown
Speed
Unknown
Apparent Right ascension
Unknown
Apparent Declination
Unknown
Sunlit
N/A
Visualization observer readout
Local Sidereal Time
18:35:53
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
455.492 km
Perigee altitude
447.915 km
Semi-major axis
6,829.841 km
Eccentricity
0.00055
Inclination
97.3536°
RAAN
90.6966°
Arg. of periapsis
265.407°
True anomaly
94.71745°
Mean anomaly
94.6541°
Eccentric anomaly
94.68578°
Mean motion
3.84527 °/min
Orbital period
93.62 mins
BSTAR
0.00032704
Loading maneuver chart data...
Computing Atmospheric mass density...

Documentation

Showing up to 5 results
|