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: 5 hours ago
TLE from 5 hours ago
0 NUSAT-49(K.VON NEUMANN)
1 60500U 24149AJ 26099.20222105 .00008331 00000-0 29209-3 0 9991
2 60500 97.3780 180.9605 0003448 151.0418 209.1014 15.29698856 91584Epoch: 2026-04-09T04:51Z
TLE epoch observation values (Epoch: 2026-04-09T04:51:11.898Z)
Latitude
-0.00007°
Longitude
-89.29269°
Altitude
481.882 km
Speed
7.623 km/s
True Right ascension
12h 03m 50s
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
15:59:07
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
476.026 km
Perigee altitude
471.301 km
Semi-major axis
6,851.801 km
Eccentricity
0.00034
Inclination
97.378°
RAAN
180.9605°
Arg. of periapsis
151.0418°
True anomaly
209.08219°
Mean anomaly
209.1014°
Eccentric anomaly
209.09179°
Mean motion
3.8268 °/min
Orbital period
94.07 mins
BSTAR
0.00029209
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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
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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. |
|---|---|---|---|---|---|---|---|
| 5 mins | 2026-04-09 17:58:58.212Z | 28.547° NE | 2026-04-09 18:00:58.212Z | 70.633° E | 35.154° | 2026-04-09 18:03:58.212Z | 170.85° S |
| 4 mins | 2026-04-10 06:06:58.212Z | 224.052° SW | 2026-04-10 06:08:58.212Z | 276.275° WNW | 22.775° | 2026-04-10 06:10:58.212Z | 315.921° NNW |
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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