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: 9 hours ago
TLE from 9 hours ago
0 NUSAT-49(K.VON NEUMANN)
1 60500U 24149AJ 25301.63727950 .00015147 00000-0 53343-3 0 9990
2 60500 97.3974 19.2280 0004327 60.3573 299.8098 15.29393359 66729Epoch: 2025-10-28T15:17Z
TLE epoch observation values (Epoch: 2025-10-28T15:17:40.948Z)
Latitude
-0.00002°
Longitude
112.58547°
Altitude
479.254 km
Speed
7.627 km/s
True Right ascension
01h 16m 54s
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
19:20:40
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
477.543 km
Perigee altitude
471.612 km
Semi-major axis
6,852.715 km
Eccentricity
0.00043
Inclination
97.3974°
RAAN
19.228°
Arg. of periapsis
60.3573°
True anomaly
299.76677°
Mean anomaly
299.8098°
Eccentric anomaly
299.78828°
Mean motion
3.82604 °/min
Orbital period
94.09 mins
BSTAR
0.00053343
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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. |
|---|---|---|---|---|---|---|---|
| 6 mins | 2025-10-29 05:32:51.606Z | 179.819° S | 2025-10-29 05:35:51.606Z | 245.908° WSW | 40.427° | 2025-10-29 05:38:51.606Z | 338.074° N |
| 5 mins | 2025-10-29 18:33:51.606Z | 343.48° N | 2025-10-29 18:35:51.606Z | 270.301° WNW | 33.564° | 2025-10-29 18:38:51.606Z | 214.254° SW |
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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