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: 22 hours ago
TLE from 22 hours ago
0 NUSAT-49(K.VON NEUMANN)
1 60500U 24149AJ 26297.16747929 .00007576 00000-0 26290-3 0 9999
2 60500 97.3713 17.5088 0002004 159.4296 200.7026 15.30071866121855Epoch: 2026-10-24T04:01Z
TLE epoch observation values (Epoch: 2026-10-24T04:01:10.210Z)
Latitude
-0.00001°
Longitude
-75.3613°
Altitude
479.988 km
Speed
7.625 km/s
True Right ascension
01h 10m 02s
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
21:32:33
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
473.921 km
Perigee altitude
471.176 km
Semi-major axis
6,850.686 km
Eccentricity
0.0002
Inclination
97.3713°
RAAN
17.5088°
Arg. of periapsis
159.4296°
True anomaly
200.69448°
Mean anomaly
200.7026°
Eccentric anomaly
200.69854°
Mean motion
3.82774 °/min
Orbital period
94.05 mins
BSTAR
0.0002629
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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. |
|---|---|---|---|---|---|---|---|
| 6 mins | 2026-10-25 05:16:03.597Z | 146.989° SSE | 2026-10-25 05:19:03.597Z | 47.98° ENE | 47.672° | 2026-10-25 05:22:03.597Z | 358.785° N |
| 5 mins | 2026-10-25 18:16:03.597Z | 21.412° NNE | 2026-10-25 18:18:03.597Z | 121.842° SE | 70.37° | 2026-10-25 18:21:03.597Z | 185.561° SSW |
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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