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: 5 hours ago
TLE from 5 hours ago
0 NUSAT-40 (C SHOEMAKER)
1 56943U 23084M 26093.31344352 .00102698 00000-0 10614-2 0 9999
2 56943 97.4793 234.6477 0004313 174.9477 185.1827 15.64412376157061Epoch: 2026-04-03T07:31Z
TLE epoch observation values (Epoch: 2026-04-03T07:31:21.520Z)
Latitude
0.00008°
Longitude
-69.84134°
Altitude
380.979 km
Speed
7.68 km/s
True Right ascension
15h 38m 35s
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
18:23:44
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
374.751 km
Perigee altitude
368.928 km
Semi-major axis
6,749.976 km
Eccentricity
0.00043
Inclination
97.4793°
RAAN
234.6477°
Arg. of periapsis
174.9477°
True anomaly
185.17824°
Mean anomaly
185.1827°
Eccentric anomaly
185.18047°
Mean motion
3.91372 °/min
Orbital period
91.98 mins
BSTAR
0.0010614
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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
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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. |
|---|---|---|---|---|---|---|---|
| 5 mins | 2026-04-03 21:53:47.231Z | 31.777° NE | 2026-04-03 21:55:47.231Z | 76.976° E | 29.292° | 2026-04-03 21:58:47.231Z | 167.701° S |
| 4 mins | 2026-04-04 09:45:47.231Z | 204.031° SW | 2026-04-04 09:46:47.231Z | 236.887° WSW | 31.055° | 2026-04-04 09:49:47.231Z | 331.152° NNW |
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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