ARMSAT1 URDANETA, 52765 (Decayed)
Orbit data source: Space-Track
ARMSAT1 URDANETA, 52765 was 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.
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52765 intel report (Beta)
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Identifier
Orbit
Country
ES / SPNRelated business
Manufacturer
Satlantis
Mission
Decayed Commercial Imaging
Bus & Motor
CUBESAT 16U, Unknown motor
Mass
15.5 kg wet, 15.5 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Box, 0.2 m
Radar Cross Section
0.100 m², Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 5 months ago
TLE from 5 months 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 16.41002704193364Epoch: 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
Visualization orbit readout
Latitude
Unknown
Longitude
Unknown
Altitude
Unknown
Speed
Unknown
Apparent Right ascension
Unknown
Apparent Declination
Unknown
Sunlit
Visualization observer readout
Local Sidereal Time
01:31:13
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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Other satellites on launch #57 in the year 2022 (2022-05-25 UTC)
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You can import UDL-sourced sensor .json files into the Sandbox to generate a visibility chart that accounts for multi-vendor sensor geometry.ARMSAT1 URDANETA Visibility
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Span | Click to sort rows by Start time (UTC) header in descending order | Start Az. | Max El. time (UTC) | Max El. Az. | Max El. | End time (UTC) | End Az. |
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| This satellite is decayed. |
Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
Click to sort rows by RSO header in ascending order | Click to sort rows by Country header in ascending order | Click to sort rows by Type header in ascending order | Click to sort rows by Inclination Δ header in ascending order | Click to sort rows by RAAN Δ header in ascending order | Click to sort rows by Coplanar Angle header in ascending order | Click to sort rows by SMA Δ header in ascending order | Click to sort rows by Orbital period header in ascending order | Click to sort rows by <5km Md TCA header in descending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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Click to sort rows by Secondary header in ascending order | Click to sort rows by Secondary name header in ascending order | Click to sort rows by Country header in ascending order | Click to sort rows by Owner header in ascending order | Click to sort rows by Obj. Type header in ascending order | Click to sort rows by Miss dist. header in ascending order | Click to sort rows by Rel. speed header in ascending order | Click to sort rows by Apr. angle header in ascending order | Click to sort rows by TCA header in descending order |
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