NUSAT-49(K.VON NEUMANN), 60500
Orbit data source: Space-Track
NUSAT-49(K.VON NEUMANN), 60500 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: 18 hours ago
TLE from 18 hours ago
0 NUSAT-49(K.VON NEUMANN)
1 60500U 24149AJ 25345.19118130 .00017918 00000-0 60273-3 0 9991
2 60500 97.3937 62.5890 0002099 240.5298 119.5734 15.30855247 73382Epoch: 2025-12-11T04:35Z
TLE epoch observation values (Epoch: 2025-12-11T04:35:18.064Z)
Latitude
0.00001°
Longitude
-86.38697°
Altitude
477.075 km
Speed
7.627 km/s
True Right ascension
04h 10m 21s
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
21:00:18
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
471.648 km
Perigee altitude
468.773 km
Semi-major axis
6,848.347 km
Eccentricity
0.00021
Inclination
97.3937°
RAAN
62.589°
Arg. of periapsis
240.5298°
True anomaly
119.59432°
Mean anomaly
119.5734°
Eccentric anomaly
119.58386°
Mean motion
3.8297 °/min
Orbital period
94 mins
BSTAR
0.00060273
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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-49(K.VON NEUMANN) 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. |
|---|---|---|---|---|---|---|---|
| 4 mins | 2025-12-12 05:50:12.711Z | 214.948° SW | 2025-12-12 05:51:12.711Z | 246.104° WSW | 30.421° | 2025-12-12 05:54:12.711Z | 326.263° NNW |
| 4 mins | 2025-12-12 18:49:12.711Z | 321.037° NNW | 2025-12-12 18:50:12.711Z | 291.54° WNW | 25.574° | 2025-12-12 18:53:12.711Z | 228.547° WSW |
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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