Showing default

NUSAT-31 (RUBY PAYNE-S), 52752

Orbit data source: Space-Track

NUSAT-31 (RUBY PAYNE-S), 52752 is a payload satellite owned by URUGUS S.A. (AR) in SSO 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.

Loading next visibility...
Identifier
52752, 2022-057W
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)
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: 5 hours ago

TLE from 5 hours ago
0 NUSAT-31 (RUBY PAYNE-S)
1 52752U 22057W   25349.99309259  .00065381  00000-0  67235-3 0  9995
2 52752  97.6428 146.0501 0002364 315.3295  44.7773 15.64679229198796
Epoch: 2025-12-15T23:50Z
TLE epoch observation values (Epoch: 2025-12-15T23:50:03.199Z)
Latitude
-0.00002°
Longitude
63.65308°
Altitude
376.172 km
Speed
7.685 km/s
True Right ascension
09h 44m 12s
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
03:08:09
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
372.674 km
Perigee altitude
369.483 km
Semi-major axis
6,749.215 km
Eccentricity
0.00024
Inclination
97.6428°
RAAN
146.0501°
Arg. of periapsis
315.3295°
True anomaly
44.79638°
Mean anomaly
44.7773°
Eccentric anomaly
44.78684°
Mean motion
3.91438 °/min
Orbital period
91.97 mins
BSTAR
0.00067235
Loading maneuver chart data...
Computing Atmospheric mass density...

Documentation

Showing up to 5 results
|