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.
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55047 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: 7 hours ago
TLE from 7 hours ago
0 NUSAT-33 (ALBANIA-2)
1 55047U 23001AQ 26035.51795587 .00013692 00000-0 51218-3 0 9991
2 55047 97.3237 99.0556 0008075 151.9469 208.2207 15.27408142172064Epoch: 2026-02-04T12:25Z
TLE epoch observation values (Epoch: 2026-02-04T12:25:51.387Z)
Latitude
-0.00001°
Longitude
137.9081°
Altitude
491.551 km
Speed
7.616 km/s
True Right ascension
06h 36m 13s
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
21:37:54
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
486.055 km
Perigee altitude
474.978 km
Semi-major axis
6,858.653 km
Eccentricity
0.00081
Inclination
97.3237°
RAAN
99.0556°
Arg. of periapsis
151.9469°
True anomaly
208.17698°
Mean anomaly
208.2207°
Eccentric anomaly
208.19884°
Mean motion
3.82107 °/min
Orbital period
94.21 mins
BSTAR
0.00051218
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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-33 (ALBANIA-2) 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. |
|---|---|---|---|---|---|---|---|
| 6 mins | 2026-02-05 04:16:28.098Z | 173.623° S | 2026-02-05 04:19:28.098Z | 221.243° SW | 43.098° | 2026-02-05 04:22:28.098Z | 342.676° N |
| 5 mins | 2026-02-05 17:18:28.098Z | 349.532° N | 2026-02-05 17:20:28.098Z | 272.754° WNW | 36.96° | 2026-02-05 17:23:28.098Z | 210.568° SW |
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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