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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 LEO that was launched on Mon, 12 Jun 2023 UTC via an FALCON 9 launch vehicle from the Air Force Western Test Range (AFWTR). Payloads include a variety of satellites, spacecraft, and rockets 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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NUSAT-42 (M WONENBURGER) details

Identifier	56966, 2023-084AL
Orbit	LEO
Last TLE update	9 hours ago
Origin	URUGUS S.A. (AR / ARGN)
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 (1 year ago)
Launch vehicle	FALCON 9
Launch site	Air Force Western Test Range (AFWTR)
Object type	Payload Rocket body Debris
Shape & HBR	Box, 0.813 m
Radar Cross Section	0.542 m², Medium (>0.1 m² and < 1m²)

Expand to show TLE details & history

TLE from 9 hours ago

0 NUSAT-42 (M WONENBURGER)
1 56966U 23084AL  24326.06238597  .00029290  00000-0  91123-3 0  9997
2 56966  97.5115  86.6558 0007145 159.1731 200.9803 15.33243745 80179

Epoch: 2024-11-21T01:29Z

Definitive object data (Epoch: 2024-11-21T01:29:50.147Z)

Latitude	-0.00009°
Longitude	3.64735°
Altitude	473.815 km
Speed	7.626 km/s
True Right ascension	05h 46m 37s
True Declination	0° 00' 00"
Sunlit	Object was in full shadow at TLE epoch

Visualization TLE readout

Latitude	0.00036°
Longitude	-175.98803°
Altitude	464.646 km
Speed	7.637 km/s
Apparent Right ascension	18h 22m 05s
Apparent Declination	-19° 23' 55"
Sunlit	Object is in daylight

Visualization observer readout

Local Sidereal Time	07:09:46
Azimuth	30.001° NE
Elevation	-67.067°
Doppler factor	1

Orbital elements

Apogee altitude	467.983 km
Perigee altitude	458.207 km
Semi-major axis	6,841.232 km
Eccentricity	0.0007145
Inclination	97.5115°
RAAN	86.6558°
Arg. of periapsis	159.1731°
True anomaly	200.95101°
Mean anomaly	200.9803°
Eccentric anomaly	200.96565°
Mean motion	3.83567 °/min
BSTAR	0.00091123
Orbital period	93.86 mins