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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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: 13 hours ago
TLE from 13 hours ago
0 NUSAT-49(K.VON NEUMANN)
1 60500U 24149AJ 26255.70386800 .00006386 00000-0 22288-3 0 9991
2 60500 97.3738 336.3710 0002224 38.8084 321.3316 15.29946766115511Epoch: 2026-09-12T16:53Z
TLE epoch observation values (Epoch: 2026-09-12T16:53:34.195Z)
Latitude
-0.00001°
Longitude
91.26946°
Altitude
477.886 km
Speed
7.627 km/s
True Right ascension
22h 25m 29s
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
22:06:37
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
474.446 km
Perigee altitude
471.399 km
Semi-major axis
6,851.059 km
Eccentricity
0.00022
Inclination
97.3738°
RAAN
336.371°
Arg. of periapsis
38.8084°
True anomaly
321.31567°
Mean anomaly
321.3316°
Eccentric anomaly
321.32364°
Mean motion
3.82742 °/min
Orbital period
94.06 mins
BSTAR
0.00022288
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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. |
|---|---|---|---|---|---|---|---|
| 5 mins | 2026-09-13 18:35:09.726Z | 353.624° N | 2026-09-13 18:37:09.726Z | 257.704° W | 55.279° | 2026-09-13 18:40:09.726Z | 205.609° SW |
| 4 mins | 2026-09-14 05:09:09.726Z | 123.035° SE | 2026-09-14 05:10:09.726Z | 90.744° ESE | 39.059° | 2026-09-14 05:13:09.726Z | 7.697° NNE |
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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