NUSAT-52, 66692
Orbit data source: Space-Track
NUSAT-52, 66692 is a payload satellite owned by URUGUS S.A. (AR) in SSO that was launched on Fri, 28 Nov 2025 UTC via an FALCON 9 launch vehicle from the Air Force Western Test Range (AFWTR). 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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66692 intel report (Beta)
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Identifier
Orbit
Country
AR / ARGNRelated business
Manufacturer
URUGUS S.A.
Mission
Operational Commercial Imaging
Bus & Motor
NEWSAT V, 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: 6 hours ago
TLE from 6 hours ago
0 NUSAT-52
1 66692U 25276AC 26238.45255703 .00004498 00000-0 20981-3 0 9991
2 66692 97.4166 310.8426 0004535 121.1438 239.0242 15.20351145 41098Epoch: 2026-08-26T10:51Z
TLE epoch observation values (Epoch: 2026-08-26T10:51:40.927Z)
Latitude
-0.00007°
Longitude
173.21673°
Altitude
509.479 km
Speed
7.608 km/s
True Right ascension
20h 43m 22s
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
08:22:14
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
504.866 km
Perigee altitude
498.626 km
Semi-major axis
6,879.883 km
Eccentricity
0.00045
Inclination
97.4166°
RAAN
310.8426°
Arg. of periapsis
121.1438°
True anomaly
238.97966°
Mean anomaly
239.0242°
Eccentric anomaly
239.00193°
Mean motion
3.8034 °/min
Orbital period
94.65 mins
BSTAR
0.00020981
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Other satellites on launch #276 in the year 2025 (2025-11-28 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-52 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 | 2026-08-26 17:44:52.363Z | 14.221° NNE | 2026-08-26 17:47:52.363Z | 172.671° S | 43.513° | 2026-08-26 17:50:52.363Z | 190.582° SSW |
| 4 mins | 2026-08-27 04:23:52.363Z | 111.122° ESE | 2026-08-27 04:24:52.363Z | 84.692° E | 26.397° | 2026-08-27 04:27:52.363Z | 14.913° NNE |
Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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