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PLATERO, 58262

Orbit data source: Space-Track

PLATERO, 58262 is a Spanish payload satellite in SSO that was launched on Sat, 11 Nov 2023 UTC via an FALCON 9 launch vehicle from the Air Force Western Test Range (AFWTR). 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
58262, 2023-174G
Orbit
SSO
Country
Flag of ESES / SPN
Related business
Manufacturer
Open Cosmos
Mission
Operational Commercial Imaging/Com
Bus & Motor
CUBESAT 6U, Unknown motor
Mass
~10 kg wet, ~10 kg dry
Launch date (UTC)
2023-11-11 (2 years ago)
Launch vehicle
FALCON 9
Launch site
Air Force Western Test Range (AFWTR)
Object type
Payload
Rocket body
Debris
Shape & HBR
Box + 2 Pan, 0.3 m
Radar Cross Section
0.098 m², Medium (>0.1 m² and < 1m²)

Expand to show TLE details & history
Last TLE update: 16 hours ago

TLE from 16 hours ago
0 PLATERO
1 58262U 23174G   25288.49031256  .00023492  00000-0  47706-3 0  9992
2 58262  97.4101  13.2060 0006338 295.5672  64.4922 15.46321334108160
Epoch: 2025-10-15T11:46Z
TLE epoch observation values (Epoch: 2025-10-15T11:46:03.005Z)
Latitude
0.00001°
Longitude
172.42984°
Altitude
428.768 km
Speed
7.655 km/s
True Right ascension
00h 52m 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
22:02:02
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
428.741 km
Perigee altitude
420.118 km
Semi-major axis
6,802.566 km
Eccentricity
0.00063
Inclination
97.4101°
RAAN
13.206°
Arg. of periapsis
295.5672°
True anomaly
64.55777°
Mean anomaly
64.4922°
Eccentric anomaly
64.52498°
Mean motion
3.86842 °/min
Orbital period
93.06 mins
BSTAR
0.00047706
Loading maneuver chart data...
Computing Atmospheric mass density...

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