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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). Payloads include a variety of satellites, spacecraft, and rockets 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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NUSAT-26 (M SOMERVILLE) details
Identifier
52184, 2022-033AD
Orbit
SSO
Last TLE update18 hours ago
Origin
Flag of ARURUGUS S.A. (AR / ARGN)
ManufacturerURUGUS S.A.
MissionOperational Commercial Imaging
Bus & MotorNEWSAT IV, Unknown motor
Mass41.5 kg wet, 38.5 kg dry
Launch date (UTC)
2022-04-01 (3 years ago)
Launch vehicle
FALCON 9
Launch site
Air Force Eastern Test Range (AFETR)
Object type
Payload
Rocket body
Debris
Shape & HBRBox, 0.813 m
Radar Cross Section0.542 m², Medium (>0.1 m² and < 1m²)

Expand to show TLE details & history

TLE from 18 hours ago
0 NUSAT-26 (M SOMERVILLE)
1 52184U 22033AD  24355.92998649  .00021219  00000-0  75551-3 0  9996
2 52184  97.2901  73.4964 0011955  28.3547 331.8341 15.28900990 21451
Epoch: 2024-12-20T22:19Z
Definitive object data (Epoch: 2024-12-20T22:19:10.832Z)
Latitude-0.00009°
Longitude8.71284°
Altitude474.976 km
Speed7.632 km/s
True Right ascension04h 53m 59s
True Declination0° 00' 00"
Sunlit
Object was in full shadow at TLE epoch
Visualization TLE readout
Latitude-82.37989°
Longitude81.44686°
Altitude510.604 km
Speed7.606 km/s
Apparent Right ascension04h 31m 53s
Apparent Declination-65° 18' 10"
Sunlit
Object is in daylight
Visualization observer readout
Local Sidereal Time15:49:40
Azimuth190.016° SSW
Elevation-63.898°
Doppler factor1
Orbital elements
Apogee altitude484.24 km
Perigee altitude467.851 km
Semi-major axis6,854.182 km
Eccentricity0.0011955
Inclination97.2901°
RAAN73.4964°
Arg. of periapsis28.3547°
True anomaly331.76935°
Mean anomaly331.8341°
Eccentric anomaly331.80173°
Mean motion3.82481 °/min
BSTAR0.00075551
Orbital period94.12 mins
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NUSAT-26 (M SOMERVILLE) Visibility forecast

Observer location: undefined°, undefined

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 mins2024-12-21 17:44:09.918Z36.876° NE2024-12-21 17:47:09.918Z107.279° ESE27.145°2024-12-21 17:49:09.918Z152.902° SSE
5 mins2024-12-22 05:52:09.918Z199.959° SSW2024-12-22 05:54:09.918Z253.212° W32.035°2024-12-22 05:57:09.918Z329.177° NNW
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