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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Edit Public Description
Identifier
Orbit
Country
Unknown / 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: 14 hours ago
TLE from 14 hours ago
0 NUSAT-40 (C SHOEMAKER)
1 56943U 23084M 26034.50155200 .00050949 00000-0 71390-3 0 9997
2 56943 97.4721 172.7184 0004389 21.4363 338.7074 15.56617174147896Epoch: 2026-02-03T12:02Z
TLE epoch observation values (Epoch: 2026-02-03T12:02:14.092Z)
Latitude
-0.00012°
Longitude
-141.52188°
Altitude
397.822 km
Speed
7.673 km/s
True Right ascension
11h 30m 52s
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
04:13:54
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
397.348 km
Perigee altitude
391.403 km
Semi-major axis
6,772.513 km
Eccentricity
0.00044
Inclination
97.4721°
RAAN
172.7184°
Arg. of periapsis
21.4363°
True anomaly
338.68913°
Mean anomaly
338.7074°
Eccentric anomaly
338.69826°
Mean motion
3.8942 °/min
Orbital period
92.45 mins
BSTAR
0.0007139
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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
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. |
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| NUSAT-40 (C SHOEMAKER) is likely not visible in the next few days. |
Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
Click to sort rows by RSO header in ascending order | Click to sort rows by Country header in ascending order | Click to sort rows by Type header in ascending order | Click to sort rows by Inclination Δ header in ascending order | Click to sort rows by RAAN Δ header in ascending order | Click to sort rows by Coplanar Angle header in ascending order | Click to sort rows by SMA Δ header in ascending order | Click to sort rows by Orbital period header in ascending order | Click to sort rows by <5km Md TCA header in descending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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