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 26102.31485884 .00017246 00000-0 39868-3 0 9998
2 56966 97.5619 243.7652 0006888 127.8623 232.3248 15.42545857157912Epoch: 2026-04-12T07:33Z
TLE epoch observation values (Epoch: 2026-04-12T07:33:23.803Z)
Latitude
-0.00004°
Longitude
-70.10556°
Altitude
444.587 km
Speed
7.644 km/s
True Right ascension
16h 15m 03s
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
20:37:12
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
440.235 km
Perigee altitude
430.848 km
Semi-major axis
6,813.678 km
Eccentricity
0.00069
Inclination
97.5619°
RAAN
243.7652°
Arg. of periapsis
127.8623°
True anomaly
232.26236°
Mean anomaly
232.3248°
Eccentric anomaly
232.29358°
Mean motion
3.85896 °/min
Orbital period
93.29 mins
BSTAR
0.00039868
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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 | 2026-04-12 22:07:29.387Z | 18.958° NNE | 2026-04-12 22:10:29.387Z | 115.775° SE | 42.2° | 2026-04-12 22:13:29.387Z | 184.154° 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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