NUSAT-32 (ALBANIA-1), 55064
Orbit data source: Space-Track
NUSAT-32 (ALBANIA-1), 55064 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.
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55064 intel report (Beta)
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Edit Public Description
Identifier
Orbit
Country
Unknown / ARGNRelated 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)
Launch vehicle
Launch site
Object type
Shape & HBR
Box, 1.0 m
Radar Cross Section
0.542 m², Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 8 hours ago
TLE from 8 hours ago
0 NUSAT-32 (ALBANIA-1)
1 55064U 23001BH 25299.30019351 .00084644 00000-0 90384-3 0 9998
2 55064 97.2112 2.2223 0005057 144.5243 215.6353 15.63638550157623Epoch: 2025-10-26T07:12Z
TLE epoch observation values (Epoch: 2025-10-26T07:12:16.719Z)
Latitude
-0.00005°
Longitude
-140.76573°
Altitude
383.09 km
Speed
7.678 km/s
True Right ascension
00h 08m 53s
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
10:14:25
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
377.471 km
Perigee altitude
370.642 km
Semi-major axis
6,752.194 km
Eccentricity
0.00051
Inclination
97.2112°
RAAN
2.2223°
Arg. of periapsis
144.5243°
True anomaly
215.60155°
Mean anomaly
215.6353°
Eccentric anomaly
215.61843°
Mean motion
3.91179 °/min
Orbital period
92.03 mins
BSTAR
0.00090384
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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.NUSAT-32 (ALBANIA-1) 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 | 2025-10-26 16:58:58.075Z | 26.459° NE | 2025-10-26 17:00:58.075Z | 93.877° ESE | 38.099° | 2025-10-26 17:02:58.075Z | 172.598° S |
| 4 mins | 2025-10-27 04:50:58.075Z | 213.298° SW | 2025-10-27 04:51:58.075Z | 242.237° WSW | 25.555° | 2025-10-27 04:54:58.075Z | 325.557° NNW |
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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