DECAYED
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NUSAT-31 (RUBY PAYNE-S), 52752 (Decayed)

Orbit data source: Space-Track

NUSAT-31 (RUBY PAYNE-S), 52752 was a payload satellite owned by URUGUS S.A. (AR) in LEO that was launched on Wed, 25 May 2022 UTC via an FALCON 9 launch vehicle from the Air Force Eastern Test Range (AFETR). 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
52752, 2022-057W
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)
2022-05-25 (4 years ago)
Launch vehicle
FALCON 9
Launch site
Air Force Eastern Test Range (AFETR)
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: 3 months ago

TLE from 3 months ago
0 NUSAT-31 (RUBY PAYNE-S)
1 52752U 22057W   26090.67473532  .10744451  27257-5  27628-3 0  9993
2 52752  97.6231 263.4280 0011332 261.5388  98.4629 16.45001178215491
Epoch: 2026-03-31T16:11Z
TLE epoch observation values (Epoch: 2026-03-31T16:11:37.131Z)
Latitude
-0.00005°
Longitude
-168.52523°
Altitude
156.881 km
Speed
7.811 km/s
True Right ascension
17h 33m 42s
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
22:01:05
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
156.741 km
Perigee altitude
141.947 km
Semi-major axis
6,527.481 km
Eccentricity
0.00113
Inclination
97.6231°
RAAN
263.428°
Arg. of periapsis
261.5388°
True anomaly
98.59131°
Mean anomaly
98.4629°
Eccentric anomaly
98.52711°
Mean motion
4.11552 °/min
Orbital period
87.47 mins
BSTAR
0.00027628
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