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: 6 hours ago
TLE from 6 hours ago
0 NUSAT-42 (M WONENBURGER)
1 56966U 23084AL 25261.33560694 .00014856 00000-0 48516-3 0 9992
2 56966 97.5396 32.1966 0008427 141.9197 218.2642 15.31825244126271Epoch: 2025-09-18T08:03Z
TLE epoch observation values (Epoch: 2025-09-18T08:03:16.439Z)
Latitude
0.00005°
Longitude
-86.12058°
Altitude
478.003 km
Speed
7.624 km/s
True Right ascension
02h 08m 47s
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
06:30:40
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
473.091 km
Perigee altitude
461.554 km
Semi-major axis
6,845.46 km
Eccentricity
0.00084
Inclination
97.5396°
RAAN
32.1966°
Arg. of periapsis
141.9197°
True anomaly
218.20445°
Mean anomaly
218.2642°
Eccentric anomaly
218.23432°
Mean motion
3.83212 °/min
Orbital period
93.94 mins
BSTAR
0.00048516
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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. |
|---|---|---|---|---|---|---|---|
| 5 mins | 2025-09-18 21:10:13.816Z | 41.611° NE | 2025-09-18 21:12:13.816Z | 86.916° E | 26.418° | 2025-09-18 21:15:13.816Z | 157.86° S |
| 4 mins | 2025-09-19 09:17:13.816Z | 212.395° SW | 2025-09-19 09:18:13.816Z | 244.128° WSW | 31.323° | 2025-09-19 09:21:13.816Z | 327.145° NNW |
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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