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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52184 intel report (Beta)
NUSAT-26 (M SOMERVILLE) details
Identifier | |
Orbit | SSO |
Last TLE update | 18 hours ago |
Origin | |
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 | Payload Rocket body Debris |
Shape & HBR | Box, 0.813 m |
Radar Cross Section | 0.542 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° |
Longitude | 8.71284° |
Altitude | 474.976 km |
Speed | 7.632 km/s |
True Right ascension | 04h 53m 59s |
True Declination | 0° 00' 00" |
Sunlit | Object was in full shadow at TLE epoch |
Visualization TLE readout
Latitude | -82.37989° |
Longitude | 81.44686° |
Altitude | 510.604 km |
Speed | 7.606 km/s |
Apparent Right ascension | 04h 31m 53s |
Apparent Declination | -65° 18' 10" |
Sunlit | Object is in daylight |
Visualization observer readout
Local Sidereal Time | 15:49:40 |
Azimuth | 190.016° SSW |
Elevation | -63.898° |
Doppler factor | 1 |
Orbital elements
Apogee altitude | 484.24 km |
Perigee altitude | 467.851 km |
Semi-major axis | 6,854.182 km |
Eccentricity | 0.0011955 |
Inclination | 97.2901° |
RAAN | 73.4964° |
Arg. of periapsis | 28.3547° |
True anomaly | 331.76935° |
Mean anomaly | 331.8341° |
Eccentric anomaly | 331.80173° |
Mean motion | 3.82481 °/min |
BSTAR | 0.00075551 |
Orbital period | 94.12 mins |
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Other satellites on launch #33 in the year 2022 (2022-04-01 UTC)
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 mins | 2024-12-21 17:44:09.918Z | 36.876° NE | 2024-12-21 17:47:09.918Z | 107.279° ESE | 27.145° | 2024-12-21 17:49:09.918Z | 152.902° SSE |
5 mins | 2024-12-22 05:52:09.918Z | 199.959° SSW | 2024-12-22 05:54:09.918Z | 253.212° W | 32.035° | 2024-12-22 05:57:09.918Z | 329.177° NNW |
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