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 26084.49908786 .00011778 00000-0 40454-3 0 9997
2 60493 97.3794 166.3647 0003839 174.2127 185.9159 15.30269689 89333Epoch: 2026-03-25T11:58Z
TLE epoch observation values (Epoch: 2026-03-25T11:58:41.191Z)
Latitude
0.00002°
Longitude
163.73155°
Altitude
480.73 km
Speed
7.624 km/s
True Right ascension
11h 05m 27s
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
23:18:02
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
474.588 km
Perigee altitude
469.328 km
Semi-major axis
6,850.095 km
Eccentricity
0.00038
Inclination
97.3794°
RAAN
166.3647°
Arg. of periapsis
174.2127°
True anomaly
185.91137°
Mean anomaly
185.9159°
Eccentric anomaly
185.91363°
Mean motion
3.82823 °/min
Orbital period
94.04 mins
BSTAR
0.00040454
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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 | 2026-03-25 18:48:39.721Z | 347.843° N | 2026-03-25 18:51:39.721Z | 278.874° WNW | 26.933° | 2026-03-25 18:53:39.721Z | 232.763° WSW |
| 5 mins | 2026-03-26 05:22:39.721Z | 161.529° S | 2026-03-26 05:24:39.721Z | 137.155° SSE | 42.779° | 2026-03-26 05:27:39.721Z | 351.814° N |
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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