Showing default

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.

Loading next visibility...
Identifier
56966, 2023-084AL
Orbit
SSO
Last TLE update
8 hours ago
Origin
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, 0.4 m
Radar Cross Section
0.542 m², Medium (>0.1 m² and < 1m²)

Expand to show TLE details & history

TLE from 8 hours ago
0 NUSAT-42 (M WONENBURGER)
1 56966U 23084AL  25199.63123411  .00009940  00000-0  34416-3 0  9999
2 56966  97.5320 329.5435 0007903  14.2395 345.9067 15.30039163116838
Epoch: 2025-07-18T15:08Z
TLE epoch observation values (Epoch: 2025-07-18T15:08:58.627Z)
Latitude
0.00005°
Longitude
165.61929°
Altitude
473.541 km
Speed
7.632 km/s
True Right ascension
21h 58m 10s
True Declination
0° 00' 00"
Sunlit
Object was in full shadow at epoch
Visualization orbit readout
Latitude
74.25434°
Longitude
13.76857°
Altitude
488.491 km
Speed
7.628 km/s
Apparent Right ascension
00h 29m 11s
Apparent Declination
39° 33' 19"
Sunlit
Object is in daylight
Visualization observer readout
Local Sidereal Time
12:14:35
Azimuth
357.139° N
Elevation
-10.459°
Doppler factor
1
Orbital elements
Apogee altitude
478.067 km
Perigee altitude
467.239 km
Semi-major axis
6,850.79 km
Eccentricity
0.00079
Inclination
97.532°
RAAN
329.5435°
Arg. of periapsis
14.2395°
True anomaly
345.88463°
Mean anomaly
345.9067°
Eccentric anomaly
345.89567°
Mean motion
3.82765 °/min
Orbital period
94.05 mins
BSTAR
0.00034416
Loading maneuver chart data...
Loading SW <> Apogee altitude chart data...
Loading historical data...
Loading historical data...
Loading historical data...
Loading historical data...
Loading historical data...
Loading historical data...
Loading historical data...
|