DECAYED
Showing default

NUSAT-43 (R DIENG-KUNTZ), 56968 (Decayed)

Orbit data source: Space-Track

NUSAT-43 (R DIENG-KUNTZ), 56968 was 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). 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
56968, 2023-084AN
Orbit
Decayed
Country
Flag of ARAR / ARGN
Related business
Manufacturer
URUGUS S.A.
Mission
Decayed 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: 2 months ago

TLE from 2 months ago
0 NUSAT-43 (R DIENG-KUNTZ)
1 56968U 23084AN  26140.16156863  .08264741  25921-5  21641-3 0  9993
2 56968  97.4278 289.3563 0015580 270.8160  89.1356 16.44357658164936
Epoch: 2026-05-20T03:52Z
TLE epoch observation values (Epoch: 2026-05-20T03:52:39.529Z)
Latitude
-0.00008°
Longitude
-6.63349°
Altitude
157.355 km
Speed
7.812 km/s
True Right ascension
19h 17m 25s
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
03:25:38
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
161.212 km
Perigee altitude
140.867 km
Semi-major axis
6,529.176 km
Eccentricity
0.00156
Inclination
97.4278°
RAAN
289.3563°
Arg. of periapsis
270.816°
True anomaly
89.31412°
Mean anomaly
89.1356°
Eccentric anomaly
89.22486°
Mean motion
4.11392 °/min
Orbital period
87.51 mins
BSTAR
0.00021641
Loading maneuver chart data...
Computing Atmospheric mass density...

Documentation

Showing up to 5 results
|