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: 16 hours ago
TLE from 16 hours ago
0 NUSAT-50 (NANCY ROMAN)
1 60493U 24149AB 26096.66029372 .00013653 00000-0 46319-3 0 9994
2 60493 97.3781 178.4529 0004620 140.0543 220.1039 15.30632239 91195Epoch: 2026-04-06T15:50Z
TLE epoch observation values (Epoch: 2026-04-06T15:50:49.377Z)
Latitude
0.00002°
Longitude
105.79898°
Altitude
479.453 km
Speed
7.625 km/s
True Right ascension
11h 53m 48s
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
13:27:44
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
474.04 km
Perigee altitude
467.711 km
Semi-major axis
6,849.012 km
Eccentricity
0.00046
Inclination
97.3781°
RAAN
178.4529°
Arg. of periapsis
140.0543°
True anomaly
220.06981°
Mean anomaly
220.1039°
Eccentric anomaly
220.08685°
Mean motion
3.82914 °/min
Orbital period
94.02 mins
BSTAR
0.00046319
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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. |
|---|---|---|---|---|---|---|---|
| 4 mins | 2026-04-07 17:31:51.714Z | 52.925° ENE | 2026-04-07 17:33:51.714Z | 94.874° ESE | 19.585° | 2026-04-07 17:35:51.714Z | 137.173° SSE |
| 5 mins | 2026-04-08 05:38:51.714Z | 186.485° SSW | 2026-04-08 05:40:51.714Z | 290.056° WNW | 40.506° | 2026-04-08 05:43:51.714Z | 340.875° 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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