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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Identifier
Orbit
Country
AR / 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: 9 hours ago
TLE from 9 hours ago
0 NUSAT-26 (M SOMERVILLE)
1 52184U 22033AD 26305.90601828 .00012241 00000-0 24297-3 0 9997
2 52184 97.2232 24.2897 0006436 102.2174 257.9798 15.47122311125962Epoch: 2026-11-01T21:44Z
TLE epoch observation values (Epoch: 2026-11-01T21:44:39.979Z)
Latitude
0.00004°
Longitude
16.93244°
Altitude
429.196 km
Speed
7.653 km/s
True Right ascension
01h 37m 09s
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
02:07:53
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
426.448 km
Perigee altitude
417.695 km
Semi-major axis
6,800.208 km
Eccentricity
0.00064
Inclination
97.2232°
RAAN
24.2897°
Arg. of periapsis
102.2174°
True anomaly
257.90768°
Mean anomaly
257.9798°
Eccentric anomaly
257.94374°
Mean motion
3.87044 °/min
Orbital period
93.01 mins
BSTAR
0.00024297
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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 | 2026-11-02 18:29:11.190Z | 356.801° N | 2026-11-02 18:31:11.190Z | 300.186° NW | 51.623° | 2026-11-02 18:34:11.190Z | 208.513° SW |
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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