Showing default

NUSAT-33 (ALBANIA-2), 55047

Orbit data source: Space-Track

NUSAT-33 (ALBANIA-2), 55047 is a payload satellite owned by URUGUS S.A. (AR) 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
55047, 2023-001AQ
Orbit
SSO
Country
Flag of UnknownUnknown / ARGN
Related business
Manufacturer
URUGUS S.A.
Mission
Operational Commercial Imaging
Bus & Motor
NEWSAT V, Unknown motor
Mass
41.5 kg wet, 38.5 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, 1.0 m
Radar Cross Section
0.542 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 NUSAT-33 (ALBANIA-2)
1 55047U 23001AQ  25346.91575095  .00017949  00000-0  68433-3 0  9995
2 55047  97.3328  46.4210 0007338   2.2507 357.8763 15.26721148163881
Epoch: 2025-12-12T21:58Z
TLE epoch observation values (Epoch: 2025-12-12T21:58:40.882Z)
Latitude
-0.00007°
Longitude
-5.09985°
Altitude
483.689 km
Speed
7.626 km/s
True Right ascension
03h 05m 41s
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
08:34:54
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
487.61 km
Perigee altitude
477.541 km
Semi-major axis
6,860.713 km
Eccentricity
0.00073
Inclination
97.3328°
RAAN
46.421°
Arg. of periapsis
2.2507°
True anomaly
357.87318°
Mean anomaly
357.8763°
Eccentric anomaly
357.87474°
Mean motion
3.81935 °/min
Orbital period
94.26 mins
BSTAR
0.00068433
Loading maneuver chart data...
Computing Atmospheric mass density...

Documentation

Showing up to 5 results
|