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: 8 hours ago
TLE from 8 hours ago
0 NUSAT-26 (M SOMERVILLE)
1 52184U 22033AD 26084.85242389 .00018063 00000-0 46669-3 0 9993
2 52184 97.2380 164.7549 0006594 173.6413 186.4918 15.39153860 91879Epoch: 2026-03-25T20:27Z
TLE epoch observation values (Epoch: 2026-03-25T20:27:29.424Z)
Latitude
0.00002°
Longitude
34.57252°
Altitude
456.205 km
Speed
7.636 km/s
True Right ascension
10h 59m 01s
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
09:29:44
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
450.043 km
Perigee altitude
441.044 km
Semi-major axis
6,823.68 km
Eccentricity
0.00066
Inclination
97.238°
RAAN
164.7549°
Arg. of periapsis
173.6413°
True anomaly
186.48326°
Mean anomaly
186.4918°
Eccentric anomaly
186.48753°
Mean motion
3.85048 °/min
Orbital period
93.49 mins
BSTAR
0.00046669
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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. |
|---|---|---|---|---|---|---|---|
| 4 mins | 2026-03-26 05:57:41.394Z | 221.138° SW | 2026-03-26 05:59:41.394Z | 273.875° WNW | 22.739° | 2026-03-26 06:01:41.394Z | 315.896° NNW |
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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