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: 17 hours ago
TLE from 17 hours ago
0 NUSAT-42 (M WONENBURGER)
1 56966U 23084AL 26155.21251869 .00025608 00000-0 54827-3 0 9992
2 56966 97.5712 298.7512 0004741 297.8133 62.2634 15.44761545166073Epoch: 2026-06-04T05:06Z
TLE epoch observation values (Epoch: 2026-06-04T05:06:01.614Z)
Latitude
-0.00007°
Longitude
-30.41554°
Altitude
433.696 km
Speed
7.652 km/s
True Right ascension
19h 55m 00s
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
08:08:52
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
432.246 km
Perigee altitude
425.792 km
Semi-major axis
6,807.156 km
Eccentricity
0.00047
Inclination
97.5712°
RAAN
298.7512°
Arg. of periapsis
297.8133°
True anomaly
62.3115°
Mean anomaly
62.2634°
Eccentric anomaly
62.28745°
Mean motion
3.86451 °/min
Orbital period
93.16 mins
BSTAR
0.00054827
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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. |
|---|---|---|---|---|---|---|---|
| 5 mins | 2026-06-04 22:45:53.516Z | 353.764° N | 2026-06-04 22:47:53.516Z | 295.58° NW | 36.07° | 2026-06-04 22:50:53.516Z | 212.254° SW |
| 4 mins | 2026-06-05 09:13:53.516Z | 131.413° SE | 2026-06-05 09:15:53.516Z | 65.59° ENE | 31.321° | 2026-06-05 09:17:53.516Z | 11.678° NNE |
| 4 mins | 2026-06-05 22:05:53.516Z | 42.111° NE | 2026-06-05 22:07:53.516Z | 113.566° SE | 31.373° | 2026-06-05 22:09:53.516Z | 163.32° 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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