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, 0.4 m
Radar Cross Section
0.542 m², Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 21 hours ago
TLE from 21 hours ago
0 NUSAT-26 (M SOMERVILLE)
1 52184U 22033AD 25256.28998655 .00010650 00000-0 36279-3 0 9994
2 52184 97.2641 334.3740 0008191 152.9736 207.1933 15.30533437 62183Epoch: 2025-09-13T06:57Z
TLE epoch observation values (Epoch: 2025-09-13T06:57:34.837Z)
Latitude
-0.00008°
Longitude
-122.54662°
Altitude
482.323 km
Speed
7.621 km/s
True Right ascension
22h 17m 29s
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
20:41:25
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
476.776 km
Perigee altitude
465.555 km
Semi-major axis
6,849.302 km
Eccentricity
0.00082
Inclination
97.2641°
RAAN
334.374°
Arg. of periapsis
152.9736°
True anomaly
207.15044°
Mean anomaly
207.1933°
Eccentric anomaly
207.17187°
Mean motion
3.8289 °/min
Orbital period
94.02 mins
BSTAR
0.00036279
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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. |
|---|---|---|---|---|---|---|---|
| 6 mins | 2025-09-14 05:03:19.046Z | 149.311° SSE | 2025-09-14 05:06:19.046Z | 76.168° E | 37.632° | 2025-09-14 05:09:19.046Z | 0.884° NNE |
| 5 mins | 2025-09-14 18:03:19.046Z | 20.387° NNE | 2025-09-14 18:05:19.046Z | 99.279° ESE | 43.472° | 2025-09-14 18:08:19.046Z | 185.231° SSW |
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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