NUSAT-40 (C SHOEMAKER), 56943 (Decayed)
Orbit data source: Space-Track
NUSAT-40 (C SHOEMAKER), 56943 was a payload satellite owned by URUGUS S.A. (AR) in LEO 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
Decayed 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: 2 months ago
TLE from 2 months ago
0 NUSAT-40 (C SHOEMAKER)
1 56943U 23084M 26257.42110219 .05621985 25837-5 55390-3 0 9997
2 56943 97.4769 53.1059 0011763 270.3114 89.6837 16.38089314182993Epoch: 2026-09-14T10:06Z
TLE epoch observation values (Epoch: 2026-09-14T10:06:23.229Z)
Latitude
0.00007°
Longitude
-91.89254°
Altitude
174.103 km
Speed
7.802 km/s
True Right ascension
03h 32m 25s
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
06:50:02
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
175.404 km
Perigee altitude
160.004 km
Semi-major axis
6,545.841 km
Eccentricity
0.00118
Inclination
97.4769°
RAAN
53.1059°
Arg. of periapsis
270.3114°
True anomaly
89.81849°
Mean anomaly
89.6837°
Eccentric anomaly
89.7511°
Mean motion
4.09822 °/min
Orbital period
87.84 mins
BSTAR
0.0005539
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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
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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. |
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| This satellite is decayed. |
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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