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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Edit Public Description
Identifier
Orbit
Country
Unknown / 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: 19 hours ago
TLE from 19 hours ago
0 NUSAT-50 (NANCY ROMAN)
1 60493U 24149AB 25309.67481054 .00014298 00000-0 48953-3 0 9992
2 60493 97.3992 27.2727 0003939 8.5001 351.6306 15.30325780 67953Epoch: 2025-11-05T16:11Z
TLE epoch observation values (Epoch: 2025-11-05T16:11:43.630Z)
Latitude
-0.00001°
Longitude
99.19683°
Altitude
475.273 km
Speed
7.63 km/s
True Right ascension
01h 49m 05s
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
06:53:59
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
474.49 km
Perigee altitude
469.093 km
Semi-major axis
6,849.928 km
Eccentricity
0.00039
Inclination
97.3992°
RAAN
27.2727°
Arg. of periapsis
8.5001°
True anomaly
351.62403°
Mean anomaly
351.6306°
Eccentric anomaly
351.62731°
Mean motion
3.82837 °/min
Orbital period
94.03 mins
BSTAR
0.00048953
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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 | 2025-11-06 17:51:49.149Z | 25.549° NE | 2025-11-06 17:54:49.149Z | 93.442° ESE | 36.135° | 2025-11-06 17:57:49.149Z | 172.203° S |
| 4 mins | 2025-11-07 05:59:49.149Z | 217.833° SW | 2025-11-07 06:01:49.149Z | 267.584° W | 23.791° | 2025-11-07 06:03:49.149Z | 312.964° NW |
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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