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, 1.0 m
Radar Cross Section
0.542 m², Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 8 hours ago
TLE from 8 hours ago
0 NUSAT-42 (M WONENBURGER)
1 56966U 23084AL 25363.85094128 .00031373 00000-0 86712-3 0 9999
2 56966 97.5484 137.0072 0007311 134.2376 225.9469 15.36956723141997Epoch: 2025-12-29T20:25Z
TLE epoch observation values (Epoch: 2025-12-29T20:25:21.326Z)
Latitude
-0.00006°
Longitude
92.1257°
Altitude
461.7 km
Speed
7.634 km/s
True Right ascension
09h 08m 01s
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
03:32:01
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
457.058 km
Perigee altitude
447.071 km
Semi-major axis
6,830.201 km
Eccentricity
0.00073
Inclination
97.5484°
RAAN
137.0072°
Arg. of periapsis
134.2376°
True anomaly
225.88673°
Mean anomaly
225.9469°
Eccentric anomaly
225.91681°
Mean motion
3.84497 °/min
Orbital period
93.63 mins
BSTAR
0.00086712
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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
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 | 2025-12-30 09:03:04.913Z | 163.342° S | 2025-12-30 09:06:04.913Z | 23.799° NE | 44.07° | 2025-12-30 09:09:04.913Z | 350.103° N |
| 4 mins | 2025-12-30 22:00:04.913Z | 9.57° NNE | 2025-12-30 22:02:04.913Z | 204.391° SW | 42.402° | 2025-12-30 22:04:04.913Z | 195.286° 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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