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: 6 hours ago
TLE from 6 hours ago
0 NUSAT-50 (NANCY ROMAN)
1 60493U 24149AB 26144.94533347 .00008130 00000-0 28789-3 0 9996
2 60493 97.3788 226.3711 0001718 280.4261 79.6786 15.29387743 98579Epoch: 2026-05-24T22:41Z
TLE epoch observation values (Epoch: 2026-05-24T22:41:16.811Z)
Latitude
-0.00001°
Longitude
3.51086°
Altitude
480.534 km
Speed
7.625 km/s
True Right ascension
15h 05m 29s
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
14:03:12
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
475.771 km
Perigee altitude
473.416 km
Semi-major axis
6,852.731 km
Eccentricity
0.00017
Inclination
97.3788°
RAAN
226.3711°
Arg. of periapsis
280.4261°
True anomaly
79.69797°
Mean anomaly
79.6786°
Eccentric anomaly
79.68828°
Mean motion
3.82602 °/min
Orbital period
94.09 mins
BSTAR
0.00028789
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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. |
|---|---|---|---|---|---|---|---|
| 5 mins | 2026-05-25 05:06:30.582Z | 140.013° SSE | 2026-05-25 05:08:30.582Z | 95.617° ESE | 33.094° | 2026-05-25 05:11:30.582Z | 6.859° NNE |
| 5 mins | 2026-05-25 18:06:30.582Z | 26.621° NE | 2026-05-25 18:08:30.582Z | 99.363° ESE | 40.855° | 2026-05-25 18:11:30.582Z | 179.821° S |
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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