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, 0.4 m
Radar Cross Section
0.542 m², Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 23 hours ago
TLE from 23 hours ago
0 NUSAT-49(K.VON NEUMANN)
1 60500U 24149AJ 25259.77642092 .00011592 00000-0 40580-3 0 9999
2 60500 97.4028 337.5474 0004772 152.3808 207.7687 15.29649638 60324Epoch: 2025-09-16T18:38Z
TLE epoch observation values (Epoch: 2025-09-16T18:38:02.767Z)
Latitude
0.00001°
Longitude
62.074°
Altitude
482.858 km
Speed
7.622 km/s
True Right ascension
22h 30m 11s
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
10:15:47
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
477.081 km
Perigee altitude
470.542 km
Semi-major axis
6,851.949 km
Eccentricity
0.00048
Inclination
97.4028°
RAAN
337.5474°
Arg. of periapsis
152.3808°
True anomaly
207.74324°
Mean anomaly
207.7687°
Eccentric anomaly
207.75597°
Mean motion
3.82668 °/min
Orbital period
94.08 mins
BSTAR
0.0004058
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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 | 2025-09-17 18:44:39.554Z | 342.885° N | 2025-09-17 18:46:39.554Z | 301.965° NW | 24.912° | 2025-09-17 18:49:39.554Z | 231.697° WSW |
| 5 mins | 2025-09-18 05:18:39.554Z | 165.787° S | 2025-09-18 05:20:39.554Z | 157.822° S | 43.828° | 2025-09-18 05:23:39.554Z | 348.874° N |
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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