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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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Identifier
52184, 2022-033AD
Orbit
SSO
Country
Flag of UnknownUnknown / ARGN
Related 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)
2022-04-01 (4 years ago)
Launch vehicle
FALCON 9
Launch site
Air Force Eastern Test Range (AFETR)
Object type
Payload
Rocket body
Debris
Shape & HBR
Box, 1.0 m
Radar Cross Section
0.542 m², Medium (>0.1 m² and < 1m²)

Expand to show TLE details & history
Last TLE update: 9 hours ago

TLE from 9 hours ago
0 NUSAT-26 (M SOMERVILLE)
1 52184U 22033AD  25286.93989325  .00019915  00000-0  64738-3 0  9997
2 52184  97.2609   4.3878 0007867  58.5876 301.6135 15.31906150 66879
Epoch: 2025-10-13T22:33Z
TLE epoch observation values (Epoch: 2025-10-13T22:33:26.776Z)
Latitude
0.00002°
Longitude
3.29076°
Altitude
470.415 km
Speed
7.632 km/s
True Right ascension
00h 17m 33s
True Declination
0° 00' 00"
Sunlit
Object was in full shadow at epoch
Visualization orbit readout
Latitude
Unknown
Longitude
Unknown
Altitude
Unknown
Speed
Unknown
Apparent Right ascension
Unknown
Apparent Declination
Unknown
Sunlit
N/A
Visualization observer readout
Local Sidereal Time
01:46:26
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
472.454 km
Perigee altitude
461.684 km
Semi-major axis
6,845.206 km
Eccentricity
0.00079
Inclination
97.2609°
RAAN
4.3878°
Arg. of periapsis
58.5876°
True anomaly
301.53669°
Mean anomaly
301.6135°
Eccentric anomaly
301.5751°
Mean motion
3.83233 °/min
Orbital period
93.94 mins
BSTAR
0.00064738
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Documentation

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