NUSAT-42 (M WONENBURGER), 56966
Orbit data source: Space-Track
NUSAT-42 (M WONENBURGER), 56966 is a payload satellite owned by URUGUS S.A. (AR) in SSO that was launched on Mon, 12 Jun 2023 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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56966 intel report (Beta)
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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: 14 hours ago
TLE from 14 hours ago
0 NUSAT-42 (M WONENBURGER)
1 56966U 23084AL 25256.30542096 .00012068 00000-0 39666-3 0 9998
2 56966 97.5397 27.0803 0008209 158.1606 201.9986 15.31668854125505Epoch: 2025-09-13T07:19Z
TLE epoch observation values (Epoch: 2025-09-13T07:19:48.37Z)
Latitude
-0.00011°
Longitude
-75.41191°
Altitude
479.15 km
Speed
7.623 km/s
True Right ascension
01h 48m 19s
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
13:40:48
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
473.409 km
Perigee altitude
462.169 km
Semi-major axis
6,845.926 km
Eccentricity
0.00082
Inclination
97.5397°
RAAN
27.0803°
Arg. of periapsis
158.1606°
True anomaly
201.9634°
Mean anomaly
201.9986°
Eccentric anomaly
201.981°
Mean motion
3.83173 °/min
Orbital period
93.95 mins
BSTAR
0.00039666
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Other satellites on launch #84 in the year 2023 (2023-06-12 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-42 (M WONENBURGER) 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 | 2025-09-13 21:59:50.971Z | 357.843° N | 2025-09-13 22:02:50.971Z | 277.339° WNW | 36.166° | 2025-09-13 22:05:50.971Z | 211.954° SW |
| 5 mins | 2025-09-14 08:33:50.971Z | 139.938° SSE | 2025-09-14 08:35:50.971Z | 67.255° ENE | 37.083° | 2025-09-14 08:38:50.971Z | 0.283° NNE |
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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