NUSAT-40 (C SHOEMAKER), 56943
Orbit data source: Space-Track
NUSAT-40 (C SHOEMAKER), 56943 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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56943 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-40 (C SHOEMAKER)
1 56943U 23084M 26144.17922696 .00074619 00000-0 58547-3 0 9992
2 56943 97.4845 288.8711 0002114 309.7067 50.4009 15.71320357165038Epoch: 2026-05-24T04:18Z
TLE epoch observation values (Epoch: 2026-05-24T04:18:05.209Z)
Latitude
-0.00001°
Longitude
-17.43569°
Altitude
357.372 km
Speed
7.695 km/s
True Right ascension
19h 15m 29s
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
07:31:13
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
353.446 km
Perigee altitude
350.601 km
Semi-major axis
6,730.161 km
Eccentricity
0.00021
Inclination
97.4845°
RAAN
288.8711°
Arg. of periapsis
309.7067°
True anomaly
50.41957°
Mean anomaly
50.4009°
Eccentric anomaly
50.41023°
Mean motion
3.93102 °/min
Orbital period
91.58 mins
BSTAR
0.00058547
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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-40 (C SHOEMAKER) 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. |
|---|---|---|---|---|---|---|---|
| 4 mins | 2026-05-24 23:11:35.917Z | 335.044° NNW | 2026-05-24 23:13:35.917Z | 286.577° WNW | 18.318° | 2026-05-24 23:15:35.917Z | 240.542° WSW |
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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