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: 6 hours ago
TLE from 6 hours ago
0 NUSAT-26 (M SOMERVILLE)
1 52184U 22033AD 25310.83906307 .00022900 00000-0 72047-3 0 9993
2 52184 97.2596 27.8277 0006016 333.5405 26.5530 15.32939022 70531Epoch: 2025-11-06T20:08Z
TLE epoch observation values (Epoch: 2025-11-06T20:08:15.049Z)
Latitude
0.00004°
Longitude
39.47337°
Altitude
466.477 km
Speed
7.635 km/s
True Right ascension
01h 51m 18s
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
22:12:41
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
468.108 km
Perigee altitude
459.875 km
Semi-major axis
6,842.128 km
Eccentricity
0.0006
Inclination
97.2596°
RAAN
27.8277°
Arg. of periapsis
333.5405°
True anomaly
26.58384°
Mean anomaly
26.553°
Eccentric anomaly
26.56842°
Mean motion
3.83492 °/min
Orbital period
93.87 mins
BSTAR
0.00072047
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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
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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. |
|---|---|---|---|---|---|---|---|
| 5 mins | 2025-11-07 05:40:01.037Z | 192.09° SSW | 2025-11-07 05:43:01.037Z | 286.97° WNW | 33.315° | 2025-11-07 05:45:01.037Z | 329.597° NNW |
| 4 mins | 2025-11-07 18:39:01.037Z | 328.652° NNW | 2025-11-07 18:40:01.037Z | 297.587° NW | 28.802° | 2025-11-07 18:43:01.037Z | 224.518° 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 ascending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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