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: 13 hours ago
TLE from 13 hours ago
0 NUSAT-40 (C SHOEMAKER)
1 56943U 23084M 26100.28284000 .00076899 00000-0 76288-3 0 9990
2 56943 97.4794 242.0431 0003872 154.4490 205.6961 15.65540383158151Epoch: 2026-04-10T06:47Z
TLE epoch observation values (Epoch: 2026-04-10T06:47:17.376Z)
Latitude
-0.00005°
Longitude
-58.29802°
Altitude
377.191 km
Speed
7.682 km/s
True Right ascension
16h 08m 10s
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
02:00:45
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
371.206 km
Perigee altitude
365.981 km
Semi-major axis
6,746.731 km
Eccentricity
0.00039
Inclination
97.4794°
RAAN
242.0431°
Arg. of periapsis
154.449°
True anomaly
205.67687°
Mean anomaly
205.6961°
Eccentric anomaly
205.68648°
Mean motion
3.91654 °/min
Orbital period
91.92 mins
BSTAR
0.00076288
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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 | 2026-04-10 22:41:01.554Z | 347.866° N | 2026-04-10 22:43:01.554Z | 288.723° WNW | 29.454° | 2026-04-10 22:45:01.554Z | 225.69° WSW |
| 4 mins | 2026-04-11 09:01:01.554Z | 122.68° SE | 2026-04-11 09:03:01.554Z | 52.635° ENE | 25.23° | 2026-04-11 09:05:01.554Z | 10.723° NNE |
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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