NUSAT-50 (NANCY ROMAN), 60493
Orbit data source: Space-Track
NUSAT-50 (NANCY ROMAN), 60493 is a payload satellite owned by URUGUS S.A. (AR) in SSO that was launched on Fri, 16 Aug 2024 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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60493 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, 1.0 m
Radar Cross Section
0.542 m², Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 1 day ago
TLE from 1 day ago
0 NUSAT-50 (NANCY ROMAN)
1 60493U 24149AB 26276.18467279 .00005264 00000-0 18390-3 0 9990
2 60493 97.3710 356.7182 0003875 147.9567 212.1910 15.29996600118648Epoch: 2026-10-03T04:25Z
TLE epoch observation values (Epoch: 2026-10-03T04:25:55.729Z)
Latitude
0.00002°
Longitude
-81.65991°
Altitude
481.176 km
Speed
7.624 km/s
True Right ascension
23h 46m 52s
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
01:26:57
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
475.428 km
Perigee altitude
470.119 km
Semi-major axis
6,850.91 km
Eccentricity
0.00039
Inclination
97.371°
RAAN
356.7182°
Arg. of periapsis
147.9567°
True anomaly
212.16735°
Mean anomaly
212.191°
Eccentric anomaly
212.17918°
Mean motion
3.82755 °/min
Orbital period
94.05 mins
BSTAR
0.0001839
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Other satellites on launch #149 in the year 2024 (2024-08-16 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-50 (NANCY ROMAN) 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 | 2026-10-04 18:39:22.841Z | 359.341° N | 2026-10-04 18:42:22.841Z | 293.913° NW | 48.663° | 2026-10-04 18:45:22.841Z | 212.521° SW |
| 5 mins | 2026-10-05 05:14:22.841Z | 137.13° SSE | 2026-10-05 05:16:22.841Z | 61.73° ENE | 46.91° | 2026-10-05 05:19:22.841Z | 0.903° 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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