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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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Identifier
56943, 2023-084M
Orbit
SSO
Country
Flag of UnknownUnknown / ARGN
Related 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)
2023-06-12 (2 years ago)
Launch vehicle
FALCON 9
Launch site
Air Force Western Test Range (AFWTR)
Object type
Payload
Rocket body
Debris
Shape & HBR
Box, 1.0 m
Radar Cross Section
0.542 m², Medium (>0.1 m² and < 1m²)

Expand to show TLE details & history
Last TLE update: 12 hours ago

TLE from 12 hours ago
0 NUSAT-40 (C SHOEMAKER)
1 56943U 23084M   25338.30355362  .00070578  00000-0  12341-2 0  9992
2 56943  97.4699 108.9701 0004718 246.5606 113.5149 15.50391719138397
Epoch: 2025-12-04T07:17Z
TLE epoch observation values (Epoch: 2025-12-04T07:17:07.032Z)
Latitude
-0.0001°
Longitude
-73.67112°
Altitude
419.992 km
Speed
7.658 km/s
True Right ascension
07h 15m 52s
True Declination
0° 00' 00"
Sunlit
Object was in full shadow at epoch
Visualization orbit readout
Latitude
Unknown
Longitude
Unknown
Altitude
Unknown
Speed
Unknown
Apparent Right ascension
Unknown
Apparent Declination
Unknown
Sunlit
N/A
Visualization observer readout
Local Sidereal Time
17:38:23
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
415.714 km
Perigee altitude
409.306 km
Semi-major axis
6,790.647 km
Eccentricity
0.00047
Inclination
97.4699°
RAAN
108.9701°
Arg. of periapsis
246.5606°
True anomaly
113.56446°
Mean anomaly
113.5149°
Eccentric anomaly
113.53968°
Mean motion
3.87861 °/min
Orbital period
92.82 mins
BSTAR
0.0012341
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