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: 3 hours ago
TLE from 3 hours ago
0 NUSAT-26 (M SOMERVILLE)
1 52184U 22033AD 26036.18957376 .00031220 00000-0 85954-3 0 9995
2 52184 97.2469 116.7216 0006336 12.4521 347.6879 15.37081772 84395Epoch: 2026-02-05T04:32Z
TLE epoch observation values (Epoch: 2026-02-05T04:32:59.172Z)
Latitude
-0.00007°
Longitude
-86.87031°
Altitude
453.631 km
Speed
7.643 km/s
True Right ascension
07h 46m 53s
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
09:50:52
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
456.008 km
Perigee altitude
447.353 km
Semi-major axis
6,829.817 km
Eccentricity
0.00063
Inclination
97.2469°
RAAN
116.7216°
Arg. of periapsis
12.4521°
True anomaly
347.67241°
Mean anomaly
347.6879°
Eccentric anomaly
347.68015°
Mean motion
3.84529 °/min
Orbital period
93.62 mins
BSTAR
0.00085954
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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 | 2026-02-05 17:37:26.015Z | 42.832° NE | 2026-02-05 17:39:26.015Z | 93.821° ESE | 27.312° | 2026-02-05 17:42:26.015Z | 160.536° S |
| 4 mins | 2026-02-06 05:41:26.015Z | 202.738° SW | 2026-02-06 05:43:26.015Z | 277.416° WNW | 32.989° | 2026-02-06 05:45:26.015Z | 327.094° NNW |
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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