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NUSAT-42 (M WONENBURGER), 56966

Orbit data source: Space-Track

NUSAT-42 (M WONENBURGER), 56966 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
56966, 2023-084AL
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 (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: 6 hours ago

TLE from 6 hours ago
0 NUSAT-42 (M WONENBURGER)
1 56966U 23084AL  26005.16535574  .00025102  00000-0  68603-3 0  9994
2 56966  97.5497 143.4942 0007397 112.5161 247.6867 15.37351512142960
Epoch: 2026-01-05T03:58Z
TLE epoch observation values (Epoch: 2026-01-05T03:58:06.735Z)
Latitude
-0.00003°
Longitude
-20.80029°
Altitude
458.977 km
Speed
7.636 km/s
True Right ascension
09h 33m 58s
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
10:14:30
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
455.945 km
Perigee altitude
445.842 km
Semi-major axis
6,829.031 km
Eccentricity
0.00074
Inclination
97.5497°
RAAN
143.4942°
Arg. of periapsis
112.5161°
True anomaly
247.60831°
Mean anomaly
247.6867°
Eccentric anomaly
247.6475°
Mean motion
3.84596 °/min
Orbital period
93.6 mins
BSTAR
0.00068603
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