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: 18 hours ago
TLE from 18 hours ago
0 NUSAT-42 (M WONENBURGER)
1 56966U 23084AL 26144.19829395 .00018478 00000-0 40448-3 0 9993
2 56966 97.5691 287.2837 0004921 345.0154 15.0947 15.44172366164372Epoch: 2026-05-24T04:45Z
TLE epoch observation values (Epoch: 2026-05-24T04:45:32.597Z)
Latitude
-0.00002°
Longitude
-25.906°
Altitude
433.692 km
Speed
7.653 km/s
True Right ascension
19h 09m 08s
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
08:03:02
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
434.102 km
Perigee altitude
427.401 km
Semi-major axis
6,808.889 km
Eccentricity
0.00049
Inclination
97.5691°
RAAN
287.2837°
Arg. of periapsis
345.0154°
True anomaly
15.10939°
Mean anomaly
15.0947°
Eccentric anomaly
15.10205°
Mean motion
3.86304 °/min
Orbital period
93.19 mins
BSTAR
0.00040448
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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. |
|---|---|---|---|---|---|---|---|
| 4 mins | 2026-05-25 08:54:19.364Z | 113.79° SE | 2026-05-25 08:56:19.364Z | 65.819° ENE | 20.701° | 2026-05-25 08:58:19.364Z | 22.831° NE |
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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