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, 0.4 m
Radar Cross Section
0.542 m², Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 14 hours ago
TLE from 14 hours ago
0 NUSAT-50 (NANCY ROMAN)
1 60493U 24149AB 25261.20833865 .00010896 00000-0 37652-3 0 9993
2 60493 97.4037 339.0118 0005119 143.6189 216.5401 15.30088767 60546Epoch: 2025-09-18T05:00Z
TLE epoch observation values (Epoch: 2025-09-18T05:00:00.459Z)
Latitude
0.00005°
Longitude
-93.36335°
Altitude
481.471 km
Speed
7.623 km/s
True Right ascension
22h 36m 02s
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
12:17:55
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
476.006 km
Perigee altitude
468.993 km
Semi-major axis
6,850.637 km
Eccentricity
0.00051
Inclination
97.4037°
RAAN
339.0118°
Arg. of periapsis
143.6189°
True anomaly
216.50519°
Mean anomaly
216.5401°
Eccentric anomaly
216.52264°
Mean motion
3.82778 °/min
Orbital period
94.05 mins
BSTAR
0.00037652
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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 | 2025-09-19 04:41:31.832Z | 119.726° SE | 2025-09-19 04:43:31.832Z | 74.377° E | 23.771° | 2025-09-19 04:46:31.832Z | 14.056° NNE |
| 5 mins | 2025-09-19 17:40:31.832Z | 40.789° NE | 2025-09-19 17:42:31.832Z | 90.478° ESE | 28.743° | 2025-09-19 17:45:31.832Z | 161.361° 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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