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: 2 days ago
TLE from 2 days ago
0 NUSAT-50 (NANCY ROMAN)
1 60493U 24149AB 26005.16498239 .00014808 00000-0 50114-3 0 9992
2 60493 97.3922 87.4956 0005009 123.3644 236.8077 15.30689689 77206Epoch: 2026-01-05T03:57Z
TLE epoch observation values (Epoch: 2026-01-05T03:57:34.478Z)
Latitude
-0.00002°
Longitude
-76.66412°
Altitude
478.739 km
Speed
7.625 km/s
True Right ascension
05h 49m 58s
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
05:26:51
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
474.135 km
Perigee altitude
467.274 km
Semi-major axis
6,848.841 km
Eccentricity
0.0005
Inclination
97.3922°
RAAN
87.4956°
Arg. of periapsis
123.3644°
True anomaly
236.75968°
Mean anomaly
236.8077°
Eccentric anomaly
236.78369°
Mean motion
3.82928 °/min
Orbital period
94.01 mins
BSTAR
0.00050114
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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 | 2026-01-07 06:18:08.925Z | 230.665° WSW | 2026-01-07 06:20:08.925Z | 269.408° W | 16.066° | 2026-01-07 06:22:08.925Z | 305.717° NW |
| 4 mins | 2026-01-07 17:44:08.925Z | 55.119° ENE | 2026-01-07 17:45:08.925Z | 83.537° E | 27.234° | 2026-01-07 17:48:08.925Z | 158.094° S |
Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
Click to sort rows by RSO header in ascending order | Click to sort rows by Country header in ascending order | Click to sort rows by Type header in ascending order | Click to sort rows by Inclination Δ header in ascending order | Click to sort rows by RAAN Δ header in ascending order | Click to sort rows by Coplanar Angle header in ascending order | Click to sort rows by SMA Δ header in ascending order | Click to sort rows by Orbital period header in ascending order | Click to sort rows by <5km Md TCA header in descending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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