NUSAT-26 (M SOMERVILLE), 52184
Orbit data source: Space-Track
NUSAT-26 (M SOMERVILLE), 52184 is a payload satellite owned by URUGUS S.A. (AR) in SSO that was launched on Fri, 01 Apr 2022 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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52184 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 IV, 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: 13 hours ago
TLE from 13 hours ago
0 NUSAT-26 (M SOMERVILLE)
1 52184U 22033AD 25340.59088398 .00027972 00000-0 84023-3 0 9991
2 52184 97.2565 57.0533 0006039 209.8945 150.1954 15.34372145 75095Epoch: 2025-12-06T14:10Z
TLE epoch observation values (Epoch: 2025-12-06T14:10:52.375Z)
Latitude
-0.00007°
Longitude
128.71865°
Altitude
469.486 km
Speed
7.629 km/s
True Right ascension
03h 48m 12s
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
01:23:40
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
463.856 km
Perigee altitude
455.597 km
Semi-major axis
6,837.863 km
Eccentricity
0.0006
Inclination
97.2565°
RAAN
57.0533°
Arg. of periapsis
209.8945°
True anomaly
150.22977°
Mean anomaly
150.1954°
Eccentric anomaly
150.21259°
Mean motion
3.83851 °/min
Orbital period
93.79 mins
BSTAR
0.00084023
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Other satellites on launch #33 in the year 2022 (2022-04-01 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-26 (M SOMERVILLE) Visibility forecast
Loading observer location...
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 | 2025-12-07 04:25:31.033Z | 103.741° ESE | 2025-12-07 04:27:31.033Z | 64.851° ENE | 15.953° | 2025-12-07 04:29:31.033Z | 28.892° NE |
| 4 mins | 2025-12-07 05:58:31.033Z | 222.652° SW | 2025-12-07 06:00:31.033Z | 274.786° WNW | 22.763° | 2025-12-07 06:02:31.033Z | 315.69° NNW |
| 4 mins | 2025-12-07 18:55:31.033Z | 323.749° NNW | 2025-12-07 18:56:31.033Z | 302.451° NW | 18.723° | 2025-12-07 18:59:31.033Z | 241.477° WSW |
Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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