NUSAT-32 (ALBANIA-1), 55064 (Decayed)
Orbit data source: Space-Track
NUSAT-32 (ALBANIA-1), 55064 was a payload satellite owned by URUGUS S.A. (AR) in LEO 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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Identifier
Orbit
Country
AR / ARGNRelated business
Manufacturer
URUGUS S.A.
Mission
Decayed 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: 2 months ago
TLE from 2 months ago
0 NUSAT-32 (ALBANIA-1)
1 55064U 23001BH 26029.11461703 .13343556 24602-5 26591-3 0 9993
2 55064 97.1663 101.3791 0008935 259.5540 100.4757 16.46665017172603Epoch: 2026-01-29T02:45Z
TLE epoch observation values (Epoch: 2026-01-29T02:45:02.911Z)
Latitude
-0.00001°
Longitude
-68.25499°
Altitude
152.465 km
Speed
7.814 km/s
True Right ascension
06h 45m 30s
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
06:08:23
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
150.749 km
Perigee altitude
139.093 km
Semi-major axis
6,523.058 km
Eccentricity
0.00089
Inclination
97.1663°
RAAN
101.3791°
Arg. of periapsis
259.554°
True anomaly
100.57636°
Mean anomaly
100.4757°
Eccentric anomaly
100.52603°
Mean motion
4.11971 °/min
Orbital period
87.38 mins
BSTAR
0.00026591
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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
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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. |
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| This satellite is decayed. |
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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