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NUSAT-29 (EDITH CLARKE), 52764

Orbit data source: Space-Track

NUSAT-29 (EDITH CLARKE), 52764 is 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
52764, 2022-057AJ
Orbit
LEO
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: 3 days ago

TLE from 3 days ago
0 NUSAT-29 (EDITH CLARKE)
1 52764U 22057AJ  25347.83508037  .09319244  25958-5  43919-3 0  9990
2 52764  97.4698 132.4978 0009872 274.3955  85.6217 16.42242227199059
Epoch: 2025-12-13T20:02Z
TLE epoch observation values (Epoch: 2025-12-13T20:02:30.943Z)
Latitude
-0.0001°
Longitude
109.11223°
Altitude
162.61 km
Speed
7.809 km/s
True Right ascension
08h 49m 59s
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
11:01:57
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
163.104 km
Perigee altitude
150.201 km
Semi-major axis
6,534.789 km
Eccentricity
0.00099
Inclination
97.4698°
RAAN
132.4978°
Arg. of periapsis
274.3955°
True anomaly
85.73451°
Mean anomaly
85.6217°
Eccentric anomaly
85.6781°
Mean motion
4.10862 °/min
Orbital period
87.62 mins
BSTAR
0.00043919
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Computing Atmospheric mass density...

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