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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.

Not visible in the next 10 days
Identifier
56943, 2023-084M
Orbit
SSO
Country
Flag of ARAR / 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 (3 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: 10 hours ago

TLE from 10 hours ago
0 NUSAT-40 (C SHOEMAKER)
1 56943U 23084M   26192.68163854  .00098663  00000-0  48990-3 0  9990
2 56943  97.4851 341.2346 0004260 193.0283 167.0876 15.81683097172670
Epoch: 2026-07-11T16:21Z
TLE epoch observation values (Epoch: 2026-07-11T16:21:33.569Z)
Latitude
-0.00003°
Longitude
166.25337°
Altitude
331.636 km
Speed
7.708 km/s
True Right ascension
22h 44m 56s
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
14:31:17
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
325.423 km
Perigee altitude
319.714 km
Semi-major axis
6,700.705 km
Eccentricity
0.00043
Inclination
97.4851°
RAAN
341.2346°
Arg. of periapsis
193.0283°
True anomaly
167.0985°
Mean anomaly
167.0876°
Eccentric anomaly
167.09305°
Mean motion
3.95697 °/min
Orbital period
90.98 mins
BSTAR
0.0004899
Loading maneuver chart data...
Computing Atmospheric mass density...

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