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ARMSAT1 URDANETA, 52765

Orbit data source: Space-Track

ARMSAT1 URDANETA, 52765 is a Spanish payload satellite 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
52765, 2022-057AK
Orbit
LEO
Country
Flag of ESES / SPN
Related business
Manufacturer
Satlantis
Mission
Operational Commercial Imaging
Bus & Motor
CUBESAT 16U, Unknown motor
Mass
15.5 kg wet, 15.5 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, 0.2 m
Radar Cross Section
0.100 m², Medium (>0.1 m² and < 1m²)

Expand to show TLE details & history
Last TLE update: 1 month ago

TLE from 1 month ago
0 ARMSAT1 URDANETA
1 52765U 22057AK  25310.85020650  .08732091  26716-5  57754-3 0  9996
2 52765  97.5887 114.2065 0008369 268.1483  91.8858 16.41002704193364
Epoch: 2025-11-06T20:24Z
TLE epoch observation values (Epoch: 2025-11-06T20:24:17.841Z)
Latitude
-0.00002°
Longitude
121.82956°
Altitude
166.568 km
Speed
7.806 km/s
True Right ascension
07h 36m 49s
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
13:23:43
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
165.423 km
Perigee altitude
154.48 km
Semi-major axis
6,538.088 km
Eccentricity
0.00084
Inclination
97.5887°
RAAN
114.2065°
Arg. of periapsis
268.1483°
True anomaly
91.98165°
Mean anomaly
91.8858°
Eccentric anomaly
91.93372°
Mean motion
4.10551 °/min
Orbital period
87.69 mins
BSTAR
0.00057754
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Computing Atmospheric mass density...

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