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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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: 7 hours ago
TLE from 7 hours ago
0 NUSAT-42 (M WONENBURGER)
1 56966U 23084AL 26095.63261014 .00031438 00000-0 73142-3 0 9993
2 56966 97.5618 236.8353 0006826 148.9675 211.1976 15.42230074156885Epoch: 2026-04-05T15:10Z
TLE epoch observation values (Epoch: 2026-04-05T15:10:57.516Z)
Latitude
-0.00001°
Longitude
175.16041°
Altitude
446.628 km
Speed
7.642 km/s
True Right ascension
15h 47m 20s
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
03:43:43
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
441.124 km
Perigee altitude
431.821 km
Semi-major axis
6,814.609 km
Eccentricity
0.00068
Inclination
97.5618°
RAAN
236.8353°
Arg. of periapsis
148.9675°
True anomaly
211.15711°
Mean anomaly
211.1976°
Eccentric anomaly
211.17735°
Mean motion
3.85817 °/min
Orbital period
93.31 mins
BSTAR
0.00073142
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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 | 2026-04-05 21:58:22.716Z | 26.198° NE | 2026-04-05 22:01:22.716Z | 122.088° SE | 35.97° | 2026-04-05 22:03:22.716Z | 171.421° S |
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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