NUSAT-48 (H. LEAVITT), 60498
Orbit data source: Space-Track
NUSAT-48 (H. LEAVITT), 60498 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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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: 8 hours ago
TLE from 8 hours ago
0 NUSAT-48 (H. LEAVITT)
1 60498U 24149AG 25342.76977459 .00016668 00000-0 58349-3 0 9996
2 60498 97.4016 60.1764 0003074 205.9208 154.1879 15.29570481 73029Epoch: 2025-12-08T18:28Z
TLE epoch observation values (Epoch: 2025-12-08T18:28:28.524Z)
Latitude
-0.00001°
Longitude
65.2935°
Altitude
482.096 km
Speed
7.623 km/s
True Right ascension
04h 00m 42s
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
01:07:47
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
476.155 km
Perigee altitude
471.942 km
Semi-major axis
6,852.185 km
Eccentricity
0.00031
Inclination
97.4016°
RAAN
60.1764°
Arg. of periapsis
205.9208°
True anomaly
154.20323°
Mean anomaly
154.1879°
Eccentric anomaly
154.19557°
Mean motion
3.82648 °/min
Orbital period
94.08 mins
BSTAR
0.00058349
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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-48 (H. LEAVITT) Visibility forecast
Loading observer location...
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 | 2025-12-09 05:35:49.403Z | 183.655° SSW | 2025-12-09 05:37:49.403Z | 222.976° SW | 38.194° | 2025-12-09 05:40:49.403Z | 335.839° NNW |
| 5 mins | 2025-12-09 18:35:49.403Z | 346.527° N | 2025-12-09 18:37:49.403Z | 283.928° WNW | 33.715° | 2025-12-09 18:40:49.403Z | 216.236° SW |
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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