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: 12 hours ago

TLE from 12 hours ago
0 BIRKELAND
1 55015U 23001G   25335.82649674  .00009680  00000-0  27963-3 0  9999
2 55015  97.3628  38.5913 0009012  95.8038 264.4233 15.35826203162016
Epoch: 2025-12-01T19:50Z
TLE epoch observation values (Epoch: 2025-12-01T19:50:09.318Z)
Latitude
-0.00006°
Longitude
30.13206°
Altitude
462.185 km
Speed
7.635 km/s
True Right ascension
02h 34m 21s
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
05:39:56
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
461.569 km
Perigee altitude
449.252 km
Semi-major axis
6,833.547 km
Eccentricity
0.0009
Inclination
97.3628°
RAAN
38.5913°
Arg. of periapsis
95.8038°
True anomaly
264.32053°
Mean anomaly
264.4233°
Eccentric anomaly
264.37191°
Mean motion
3.84215 °/min
Orbital period
93.7 mins
BSTAR
0.00027963
Loading maneuver chart data...
Computing Atmospheric mass density...

Documentation

Showing up to 5 results
|