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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: 7 hours ago

TLE from 7 hours ago
0 NUSAT-42 (M WONENBURGER)
1 56966U 23084AL  26052.83879389  .00019457  00000-0  49307-3 0  9991
2 56966  97.5541 192.5792 0006036 304.9379  55.1299 15.39742408150291
Epoch: 2026-02-21T20:07Z
TLE epoch observation values (Epoch: 2026-02-21T20:07:51.792Z)
Latitude
0.00001°
Longitude
98.85777°
Altitude
447.629 km
Speed
7.645 km/s
True Right ascension
12h 50m 19s
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
06:08:21
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
447.934 km
Perigee altitude
439.699 km
Semi-major axis
6,821.953 km
Eccentricity
0.0006
Inclination
97.5541°
RAAN
192.5792°
Arg. of periapsis
304.9379°
True anomaly
55.18667°
Mean anomaly
55.1299°
Eccentric anomaly
55.15828°
Mean motion
3.85194 °/min
Orbital period
93.46 mins
BSTAR
0.00049307
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