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: 19 hours ago
TLE from 19 hours ago
0 NUSAT-49(K.VON NEUMANN)
1 60500U 24149AJ 25315.17887675 .00016356 00000-0 56810-3 0 9990
2 60500 97.3967 32.7011 0003430 20.9605 339.1775 15.29829561 68793Epoch: 2025-11-11T04:17Z
TLE epoch observation values (Epoch: 2025-11-11T04:17:34.951Z)
Latitude
-0.00005°
Longitude
-82.26367°
Altitude
477.227 km
Speed
7.628 km/s
True Right ascension
02h 10m 48s
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
20:09:00
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
475.624 km
Perigee altitude
470.924 km
Semi-major axis
6,851.411 km
Eccentricity
0.00034
Inclination
97.3967°
RAAN
32.7011°
Arg. of periapsis
20.9605°
True anomaly
339.16352°
Mean anomaly
339.1775°
Eccentric anomaly
339.17051°
Mean motion
3.82713 °/min
Orbital period
94.07 mins
BSTAR
0.0005681
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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 | 2025-11-12 05:32:00.411Z | 178.809° S | 2025-11-12 05:35:00.411Z | 261.476° W | 41.555° | 2025-11-12 05:38:00.411Z | 339.903° N |
| 5 mins | 2025-11-12 18:32:00.411Z | 352.371° N | 2025-11-12 18:34:00.411Z | 303.597° NW | 34.665° | 2025-11-12 18:37:00.411Z | 216.23° 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 ascending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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